Systems, Methods and Computer-Readable Media for Improving Platform Guidance or Navigation Using Uniquely Coded Signals

ABSTRACT

A spatially-distributed architecture (SDA) of antennas transmits respective uniquely coded signals. A first receiver having a known position in a coordinate system defined by the SDA receives reflected versions of the uniquely coded signals. A first processor receives the reflected versions of the uniquely coded signals and identifies a position of a non-cooperative object in the coordinate system. A platform with a platform receiver receives non-reflected versions of the uniquely coded signals. The platform determines a position of the platform in the coordinate system. In an example, the platform uses a self-determined position and a position of the non-cooperative object communicated from the SDA to navigate or guide the platform relative to the non-cooperative object. In another example, the platform uses a self-determined position and information from an alternative signal source in a second coordinate system to guide the platform. Guidance solutions may be generated in either coordinate system.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Continuation of U.S. non-provisional application,assigned Ser. No. 15/654,270, filed Jul. 19, 2017, entitled, “Systems,Methods and Computer-Readable Media for Improving Platform Guidance orNavigation Using Uniquely Coded Signals,” which application was aContinuation-In-Part of U.S. non-provisional patent application,assigned application Ser. No. 15/641,079, filed Jul. 3, 2017, having thesame title; and U.S. non-provisional patent application, assignedapplication Ser. No. 15/140,381, filed Apr. 27, 2016, having the sametitle (which application became U.S. Pat. No. 9,696,418, whichapplications claimed the benefit of the filing date of a provisionalpatent application assigned application Ser. No. 62/156,880, filed onMay 4, 2015, entitled “A Method for Improving Commanded PlatformGuidance Using Coded Signals,” the entire contents of these applicationsare incorporated herein by reference.

TECHNICAL FIELD

The invention relates to systems and methods for determining theposition and relative motion (if any) of a non-cooperative object andthe position and relative motion of a cooperative platform while guidingor navigating the cooperative platform relative to the non-cooperativeobject.

BACKGROUND

Command guidance fire control systems are used to guide a missile into atarget. Command guidance fire control systems track the position andmotion of the missile and of the target while controlling the flightpath of the missile to cause it to intercept the target. The missile isoften referred to as an interceptor or interceptor platform. The targetis a “non-cooperative object,” and will be referred to hereininterchangeably as a target or as a non-cooperative object. The commandguidance fire control system includes one or more radar systems locatedat a fire control sensor station of the command guidance fire controlsystem. The fire control sensor station may be fixed (e.g., when locatedon or in a structure or structures) or unfixed (e.g., when located on orin a non-moving vehicle) or the fire control sensor station may belocated on a moving platform, such as a ship, a tank, an airplane, etc.The command guidance fire control system also includes a receiverlocated on the interceptor platform and a transmitter located at thefire control sensor station.

The radar system transmits radar signals from the fire control sensorstation. The radar system includes a radar sensor that detects radarsignals reflected off of the non-cooperative object and off of theinterceptor platform. A processor of the fire control sensor stationprocesses the detected radar signals and determines the position andmotion of the target and of the interceptor platform. The processor thencomputes a guidance solution. The transmitter located at thefire-control station transmits the guidance solution to the receiverlocated on the interceptor platform. The guidance solution is processedby a processor on the interceptor platform that causes the flight pathof the interceptor platform to be adjusted, if necessary, to maintain aflight path that will intercept the target, or non-cooperative object.

One of the problems inherent in a conventional command guidance firecontrol system attempting to intercept a target is that the computationof the guidance solution at the fire-control sensor station and thecommunication of the guidance solution to the interceptor platformintroduce excessive time delays between the time of determining targetposition and motion and the time of guidance solution command executionon the interceptor platform. These delays are attributed to: 1) the timethat is required for the fire control sensor station to detect anddetermine the separate position and motion of both the target and theinterceptor platform: 2) the time that is required for the fire controlsensor station to compute the guidance solution in a coordinate frameconvenient for the interceptor platform to execute guidance solutioncommands; 3) the time that is required for the guidance solution to becommunicated from the fire control sensor station to the interceptorplatform; and 4) the time that is required for the interceptor platformto process the received communication.

For the fire control sensor station to determine accurate guidancecommands in a coordinate frame convenient or suitable for use by theinterceptor platform, the fire control sensor station must haveknowledge about the orientation of the interceptor platform, whichrequires time and resources that can degrade the efficiency of thefire-control sensor station. Also, the requirement for the fire controlsensor station to track the interceptor platform can introduce errors inthe position and motion of the interceptor platform due to a lack of astable reflection from the interceptor platform. These errors, in turn,introduce two-way path signal propagation spreading losses that imposesignal-to-noise requirements on the command guidance fire control systemthat may be difficult to meet.

To address the time delay problems associated with conventional commandguidance fire control systems, methods have been used to enhanceguidance solution processing at the fire control sensor stationprocessor and to improve the communication links between the firecontrol sensor station and the interceptor platform. One conventionalmethod for aligning the coordinate frame of the interceptor platformwith the coordinate frame of the fire control station requires that thefire control sensor station track the motion of the interceptor platformthrough one or more maneuvers. These jink maneuvers include one or morechanges of direction to allow the fire control sensor station's estimateof the interceptor platform velocity vector to be aligned with anonboard inertial sensor estimate of the interceptor platform velocity,but generally require either communicating the interceptor platformvelocity from the interceptor platform to the fire control sensor orcommunicating the fire control sensor station's estimate of interceptorplatform velocity to the interceptor platform and performing thealignment computation in the interceptor platform processor. In eithercase, the coordinate alignment adds complexity and processingrequirements to the command guidance fire control system.

Other solutions for addressing these issues have introduced active andsemi-active seekers onboard the interceptor platform to compute theposition and motion of the non-cooperative object on the interceptorplatform. While these systems mitigate timing delays and eliminate theneed for jink maneuvers, they introduce another level of complexity thatcan impact overall system cost. In particular, these seeker solutionsrequire alignment and calibration of the onboard sensor hardware withthe on-board inertial navigation hardware that can add to complexity andcost.

In general, the existing solutions incur significant time delays due toincreases in processing overhead and information sharing requirementsbetween the fire control sensor station and the interceptor platformand/or increase onboard interceptor platform hardware complexity andcost.

U.S. Pat. No. 8,120,526 (hereinafter “the '526 patent”), which isassigned to the applicant of the present application and which disclosesinventions that were invented by the inventor of the presentapplication, discloses a guidance system in which the interceptorplatform is capable of self-determining its own position and motion andthe position and motion of the target, or non-cooperative object, usingcoded signals. While the '526 patent includes significant improvementsover the above-described conventional systems, complexity and costs dueto processing overhead requirements remain.

SUMMARY

Improved systems for locating, guiding or navigating platforms aredisclosed. In some embodiments, a common coordinate system consisting ofat least two orthogonal axes is used to avoid the above-describedcomplexities in conventional guidance and fire control systems. Someapplications define and apply a two-axis coordinate system to describeposition, motion and orientation, while some other applications willcall for a common or first coordinate system consisting of a three-axiscoordinate system. Such a three-axis coordinate system will consist ofthree orthogonal (or substantially orthogonal) axes.

Embodiments of the improved systems include a spatially-distributedarchitecture (SDA) of antenna arrays that transmit a set of uniquelycoded signals. Each antenna array in the SDA of antenna arrays has aknown position in a first coordinate system. A first receiver having aknown position in the first coordinate system defined by the SDA ofantenna arrays receives reflections of the uniquely coded signalsreflected by an object. One or more characteristics of the uniquelycoded signals present in the reflected versions received by the firstreceiver are forwarded to a first processor. The first processorreceives electrical signals representative of the reflected versions ofthe uniquely coded signals from the first receiver and identifies atleast a position of the object in the first coordinate system. Aplatform, separate from both the SDA and first receiver, includes asecond or platform receiver that receives non-reflected versions of theuniquely coded signals. A platform processor determines at least aposition of the platform in the first coordinate system.

An alternative embodiment includes a first receiver having a knownposition in a first coordinate system, a first processor incommunication with the first receiver, a platform separate from thefirst receiver. The first receiver receives reflections of a set ofuniquely coded or uniquely identifiable signals transmitted from aspatially-distributed architecture (SDA) of antenna arrays having aknown position in the first coordinate system. The platform is arrangedwith a second or platform receiver that directly receives the set ofuniquely coded signals from the SDA of antenna arrays. The platformprocessor is in communication with the second or platform receiver andin response to information from the second or platform receiverdetermines a position of the platform in the first coordinate system.

Another example embodiment includes a method for locating at least onenon-cooperative object and communicating the location of the at leastone non-cooperative object, the method includes the steps of: receiving,with a receiver having a known position in a coordinate system,reflected versions of respective uniquely identifiable signalstransmitted from a set of spatially-separated antenna arrays therespective positions of which are known in the coordinate system, wherethe reflected versions are reflected from a non-cooperative object;determining, with a processor in communication with the receiver, alocation of the non-cooperative object, the determining based on one ormore characteristics of the reflected versions of the uniquelyidentified signals; and communicating, from the processor incommunication with the receiver, one of the characteristics of thereflected versions of the uniquely identified signals or the location ofthe of the non-cooperative object in the coordinate system.

Still another example embodiment includes a method for self-determiningone or more of a position, a motion, and an orientation of a platform ina coordinate system and generating a guidance solution, the methodincluding the steps of receiving, with a first receiver connected to aplatform, a set of uniquely identifiable signals transmitted fromrespective spatially-distributed antenna arrays removed from theplatform; determining, with a platform processor in communication withthe first platform receiver, one or more of a position, a motion and anorientation of the platform, wherein the platform processor identifiesat least one of the position, motion and orientation of the platformusing one or more characteristics of the uniquely identified signalsreceived by the first receiver; receiving, one or more signalscontaining information about a relative position of a non-cooperativeobject, wherein the information about the relative position of thenon-cooperative object is communicated in an established externalinertial frame or the first coordinate system defined by thespatially-distributed architecture of antenna arrays; generating, withthe platform processor, a guidance solution responsive to the relativeposition of the non-cooperative object; and applying at least onecontrol signal responsive to the guidance solution to direct theplatform relative to the non-cooperative object.

In some embodiments, the example method described above may furtherinclude periodically receiving an informational signal identifying apresent location of one or more of the antenna arrays or a position in acoordinate system relative to the location of the antenna arrays andadjusting a location of the platform responsive to the present locationof the one or more of the antenna arrays and a platform determinedposition from one or more characteristics of the uniquely identifiedsignals received by the first receiver.

In some other example embodiments, the example method may alternativelyinclude generating a platform unique signal different from any member ofthe set of uniquely identifiable signals transmitted from the antennaarrays, transmitting the platform unique signal and periodicallytransmitting an informational signal identifying a present location ofthe platform.

Another example embodiment includes a receiver system at a knownlocation in a coordinate system for guiding remote forward-basedplatforms, the receiver system comprising an antenna, a transceivercoupled to the antenna and arranged to receive reflected versions of aset of uniquely identifiable signals transmitted from a respective setof spatially-distributed antenna arrays where the reflected versions arereflected by a non-cooperative object, a processor communicativelycoupled to the transceiver and arranged to determine at least a positionof the non-cooperative object in the coordinate system based on arespective time of arrival and phase of the reflected versions of theuniquely identified signals and an angular position and a range of thetransceiver relative to an origin of the first coordinate system.

Another example embodiment includes a remote or forward-based platformthat directly receives a set of uniquely identifiable signalstransmitted from a respective set of spatially-distributed antennaarrays. A transceiver converts electromagnetic energy responsive to theset of uniquely identifiable signals to a first set of correspondinginput signals. A processor uses a respective time of arrival and phasefrom the set of corresponding input signals to determine at least aposition of the forward-based platform in a first coordinate systemdefined by the set of spatially-distributed antenna arrays. Theforward-based platform also receives information concerning a positionof a non-cooperative object separate from the forward-based platform.There are at least three separate and distinct mechanisms for theforward-based platform to receive the information signal(s).

In a first mechanism, a receiver system communicatively coupled to thespatially-distributed architecture (SDA) of antenna arrays receivesreflected versions of the set of uniquely identifiable signals that arereflected from the non-cooperative object. A processor coupled to thereceiver system determines a position of the non-cooperative objectusing the reflected versions and the arrangement of the SDA of antennaarrays to identify the location of the non-cooperative object in acoordinate system defined by the SDA of antenna arrays. The processorforwards one or more signals that identify the position, orientation andmotion (if any) of the non-cooperative object via one or moreinformation signals separate and distinct from the set of uniquelyidentifiable signals to the forward-based platform.

In a second mechanism, a receiver system that is indirectly coupled tothe SDA of antenna arrays receives one or more signals from thenon-cooperative object. The received signals can operate in one or morespectra including but not limited to electro-optical, infra-red,radio-frequency, acoustic, or sonar. A processor coupled to the receiversystem determines a position of the non-cooperative object using thereceived signals to identify the location of the non-cooperative objectin a second coordinate system other than that defined by the SDA ofantenna arrays. The processor forwards one or more signals that identifythe position, orientation and motion (if any) of the non-cooperativeobject via one or more information signals separate and distinct fromthe set of uniquely identifiable signals to the forward-based platform.The coordinate system of the non-cooperative object's position,orientation, and motion are converted into the first coordinate systemby one or more processors associated with the SDA of antenna arrays.

In addition or alternatively, the remote platform (which may bestationary or mobile) may be arranged with a sensor or sensor subsystemthat provides one or more information signals to a platform processor.The one or more information signals include a range and one or moreangles with respect to the planes defined by the coordinate systemdefined by the SDA of antenna arrays. Still further, the remote platformmay receive one or more information signals identifying the location ofthe non-cooperative object from one or more off platform signal sources.When the remote signal sources forward information in a secondcoordinate system different from the coordinate system defined by theSDA of antenna arrays, the remote or forward-based platform will performa coordinate conversion before determining any necessary control signalsto guide or navigate the platform with respect to the non-cooperativeobject. Otherwise, when the remote signal source provides locationinformation in the same coordinate system being used by the systemdirecting the SDA of antenna arrays a coordinate conversion may beavoided.

In some embodiments, the forward-based platform is arranged with aninertial navigation system that provides a position, orientation andvelocity of the platform to the platform processor. The forward-basedplatform directly receives a set of uniquely identifiable signalstransmitted from a respective set of spatially-distributed antennaarrays arranged on a pilot platform separate from the forward-basedplatform. A transceiver on the forward-based platform convertselectromagnetic energy responsive to the set of uniquely identifiablesignals to a first set of corresponding input signals. A platformprocessor uses a respective time of arrival and phase from the set ofcorresponding input signals and the spatial relationships between theantenna arrays to determine at least a position and velocity vector ofthe forward-based platform in a first coordinate system defined as aninertial frame or by the set of spatially distributed antenna arrays.The processor uses the pilot platform position, velocity vector, andinformation from the inertial navigation system to align the inertialsensor second coordinate frame with the first coordinate frame definedby the pilot platform. The information from one or more sensors or asensor subsystem is communicated to each interceptor platform in thefirst coordinate frame to generate a guidance solution and direct therespective interceptor platform relative to the non-cooperative object.The forward-based platform also receives a periodic information signalidentifying a present position of each of the antenna arrays in thespatially-distributed architecture. The periodic information signal canbe used by a platform processor to verify the accuracy of the positionand orientation information in the platform's inertial navigationsystem. When so desired, information in the periodic signal can be usedto replace and/or adjust the position and orientation information in theplatform's inertial navigation system.

In these alternative embodiments, the forward-based platform may beaccompanied by or within communication range of one or more interceptorplatforms. The interceptor platforms will be similarly arranged with oneor more antennas, a transceiver and a platform processor suitable forreceiving the set of uniquely coded signals from thespatially-distributed architecture of antenna arrays and determining arespective position, orientation and motion (if any) in the coordinatesystem defined by the physical arrangement of the spatially-distributedarchitecture of antenna arrays. The interceptor platforms may be furtherarranged with control and or guidance systems to direct or navigate theinterceptor platform relative to the non-cooperative object. Each of theinterceptor platforms may be arranged without a respective sensor orsensor subsystem that would enable each interceptor platform toautonomously determine the location of the non-cooperative object butmay be arranged with a respective sensor or sensor system thatdetermines some components of position of the non-cooperative objectsuch as range and not angle, or angle and not range. When theforward-based platform is within communication range of one or moreinterceptors, the interceptors can communicate information to theforward-based platform and the forward-based platform may communicateinformation about the non-cooperative target and the forward-basedplatform's present position and orientation in the coordinate systemdefined by the SDA of antenna arrays. The interceptor platforms may alsoreceive the periodic information signal identifying a present positionof each of the antenna arrays in the SDA. The SDA of antenna arraysdefines a first coordinate system that is either located on the ground,on the surface of a body of water or on aerial platform(s). When the SDAis located on a mobile platform the periodic information signal can bereceived directly from the system managing the SDA of antenna arrays orindirectly via the forward-based platform. However received, theperiodic information signal is used by a respective interceptor platformprocessor to verify the accuracy of the position and orientationinformation in the inertial navigation system. When so desired,information in the periodic information signal can be used to replaceand/or adjust the position and orientation information in the inertialnavigation system.

Other alternative embodiments of a system of platforms are contemplated.A pilot platform emits a set of uniquely identifiable signals from aprimary SDA of antenna arrays. The spatial relationships between theseparate antenna arrays of the spatially-distributed architecture areknown and fixed relative to one another when the primary SDA isterrestrially based or deployed on a single vehicle or forward-basedplatform. A set of forward-based platforms that may or may not be mobileare separate from the pilot platform receive the uniquely identifiablesignals from the spatially-distributed architecture of antenna arrays.Each forward-based platform includes a platform processor thatdetermines one or more of a remote or forward-based platform position,orientation and motion with respect to a coordinate system defined bythe primary SDA of antenna arrays. Two or more forward-based platformsare arranged with a signal generator that generates a remote orforward-based platform uniquely identifiable signal different from themembers of the set of uniquely identifiable signals sent from theprimary SDA of antenna arrays. A transceiver receives, processes, andforwards the platform uniquely identifiable signal to a remote platformantenna arranged to transmit the remote platform uniquely identifiablesignal in a direction other than toward the pilot platform. Atransmitted version of the remote platform uniquely identifiable signalis a component signal of a remote or secondary SDA of antenna arraysseparate from the primary SDA of antenna arrays.

In addition, an interceptor platform directly receives a set of uniquelyidentifiable signals transmitted from the forward-based platforms. Atransceiver on the interceptor platform converts electromagnetic energyresponsive to the set of uniquely identifiable signals to a first set ofcorresponding input signals. A platform processor uses a respective timeof arrival and phase from the set of corresponding input signals and thespatial relationships between the antenna arrays on the one or moreforward-based platforms to determine at least a position of theinterceptor platform in a first coordinate system defined by the set ofspatially distributed antenna arrays. Each forward-based platform isfurther arranged to transmit one or more informational signals. Theinformational signals may include information about the respectivelocations and orientations of the forward-based platforms. Theinformational signals from each of the members of the forward-basedplatforms coupled with the platform unique signals being transmittedfrom each of the members creates a secondary spatially-distributedarchitecture of antenna arrays that can be used by one or moreinterceptor platforms to determine their respective locations in thecoordinate system defined by the secondary SDA of antenna arrays.

Interceptor platforms may be arranged to receive and process reflectionsof the uniquely identifiable signals sent from the (primary) SDA ofantenna arrays to determine one or more of a position, orientation andmotion (if any) of a non-cooperative object responsible for thereflections. Alternatively, or in addition, interceptor platforms may bearranged to receive and process reflections of the forward-basedplatform unique signals sent from the remote or secondary SDA of antennaarrays to determine one or more of a position, orientation and motion(if any) of a non-cooperative object responsible for the reflections.Moreover, one or more forward-based platform and/or one or moreinterceptor platform may be arranged with one or more sensors or sensorsubsystems that identify a location of a non-cooperative object.Forward-based platforms and interceptor platforms may share informationconcerning the location, orientation and motion (if any) of thenon-cooperative object in addition to information concerning theirrespective location in either the coordinate system defined by theprimary SDA of antenna arrays or the secondary SDA of antenna arrays asdesired. Such shared information may include range only, one or moreangles only (in one or more of the X-Y, X-Z and Y-Z planes), orcombinations of range and one or more angles. When known and so desired,the shared information may include X, Y and Z coordinates in acoordinate system defined by the primary SDA of antenna arrays.Alternatively, the shared information may be communicated in an inertialframe (e.g., a location, orientation and velocity vector) in anestablished external inertial frame independent of the SDA or antennaarrays and independent of the motion of the platform or platforms.

Another example embodiment includes a non-transitory computer-readablemedium having code stored thereon for execution by a processor in asensor system, the computer-readable medium comprising a transmit modulearranged to communicate a set of uniquely identifiable signals to a SDAof N antenna arrays, where N is a positive integer greater than or equalto two, the SDA of N antenna arrays defining a first coordinate system;a receive module coupled to a first receiver located at a known positionin the first coordinate system where the first receiver, receivesreflected versions of the set of uniquely identifiable signalstransmitted from the SDA of N antenna arrays and reflected by thenon-cooperative object, determines a location of the non-cooperativeobject in the first coordinate system based on a respective time andphase of reflected versions of the uniquely identified signals and anangular position and a range of the first receiver relative to an originof the first coordinate system, and forwards an information signalcontaining the location of the non-cooperative object in the firstcoordinate system.

Another embodiment includes a non-transitory computer-readable mediumhaving executable code stored thereon for execution by a processor, thecomputer-readable medium comprising: a locator module integrated in amovable platform and arranged to receive a first set of signalsresponsive to non-reflected versions of a set of uniquely identifiablesignals transmitted from a SDA of N antenna arrays, where the locatormodule determines one or more of a platform position, motion andorientation from spatial relationships of the N antenna arrays and arespective time of arrival and phase of the first set of signals in thefirst coordinate system; and a second module arranged to receive one ormore of the position, motion and orientation of the platform from thelocator module and the position and motion of the non-cooperative objectfrom a signal source remote from the movable platform, where the secondmodule generates one or more control signals to direct the movableplatform with respect to the non-cooperative object.

A set of uniquely identifiable signals and or unique coded signals mayinclude one or more mechanisms or signal processing techniques forgenerating and transmitting over the air radio-frequency electromagneticsignals that can be distinguished from each of the other members of aset of signals. Example mechanisms or signal processing techniquesinclude time-division multiplexing, frequency-division multiplexing,code-division multiplexing, and polarization orientation coding. Forsome environments, a combination of one or more of these techniques canbe used to generate a set of signals that do not interfere or minimallyinterfere with one another and are thus separately identifiable.

BRIEF DESCRIPTION OF THE DRAWINGS

Improved systems, methods and computer-readable media can be betterunderstood with reference to the following drawings. Components anddistances between components in the drawings are not necessarily toscale, emphasis instead being placed upon clearly illustrating theprinciples involved.

FIG. 1 is a functional block diagram of an example embodiment of anenvironment in which a sensor system uses coded signals to guide aplatform or platforms relative to a non-cooperative object or target.

FIG. 2A is a schematic diagram of an example embodiment of the spatiallydistributed architecture (SDA) introduced in the sensor system of FIG.1.

FIG. 2B is a schematic diagram illustrating an alternative embodiment ofthe SD architecture of FIG. 1.

FIG. 3A is a schematic diagram of an example embodiment of the firstreceiver of FIG. 1.

FIG. 3B is a schematic diagram of an alternative embodiment of the firstreceiver of FIG. 1.

FIG. 4A is a schematic diagram of an example embodiment of a platformintroduced in FIG. 1.

FIG. 4B is a schematic diagram of an alternative embodiment of theplatform of FIG. 1.

FIG. 5 is a schematic diagram that illustrates the manner in which theposition and orientation of a target or non-cooperative object relativeto the receiver of FIG. 1 can be determined in two dimensions.

FIG. 6 is a schematic diagram that illustrates the manner in which theposition and orientation of the second receiver relative to the SDA ofFIG. 1 can be determined in two dimensions.

FIG. 7 is a schematic diagram that illustrates the manner in which theposition and orientation of the second receiver relative to the SDA ofFIG. 1 can be determined in three dimensions.

FIG. 8 is a schematic diagram that illustrates spatial relationships inan example arrangement of a SDA, receiver and a non-cooperating objectof FIG. 1 in two dimensions.

FIG. 9 is a schematic diagram that illustrates spatial relationships inan example arrangement of a SDA, a receiver with multiple antennas and anon-cooperative object of FIG. 1 in two dimensions.

FIG. 10 is a flow diagram illustrating an example embodiment of a methodfor locating a non-cooperative object relative to a platform.

FIG. 11 is a flow diagram illustrating an example embodiment of a methodfor self-determining one or more of a position, motion and orientationin a coordinate system and guiding a platform relative to a remotenon-cooperative object.

FIG. 12 includes a flow diagram illustrating an example embodiment of amethod for self-determining one or more of a position, motion andorientation in a first coordinate system on a platform and using one ormore signals containing information about a non-cooperative object toguide the platform relative to a non-cooperative object.

FIG. 13 is a flow diagram illustrating an alternative embodiment of themethod introduced in FIG. 12.

FIG. 14 is a schematic diagram that illustrates an embodiment of asystem of platforms including a group of forward-based platformsnavigating in accordance with location information from a SDA of antennaarrays.

FIG. 15 is a schematic diagram that illustrates another alternativeembodiment of a system of platforms including a group of interceptorplatforms navigating in accordance with a separate or secondary SDA ofantenna arrays.

DETAILED DESCRIPTION OF ILLUSTRATED EMBODIMENTS

In accordance with illustrative or exemplary embodiments describedherein, a spatially-distributed architecture (SDA) of antenna arrays orsignal subsystem transmits a set of N uniquely coded electromagneticsignals and receives information from reflected versions of the set of Nuniquely-coded signals. The SDA of antenna arrays may be ground basedand fixed in position with respect to one another. Alternatively, theSDA of antenna arrays may be mobile and distributed across one or moresurfaces of a mobile platform such as a vehicle, ship, plane, or othermobile platform. Furthermore, in some alternative embodiments, antennaarrays may be deployed on separate mobile platforms to form a remote orsecondary SDA of antenna arrays.

When reflected versions of the set of N uniquely-coded signals arereceived by or communicated to the SDA of antenna arrays or signalsubsystem, the position and motion (if any) of a non-cooperative objector target in a coordinate system defined by the SDA of antenna arrays isdetermined by comparing one or more characteristics of the reflectedversions of the set of N uniquely-coded signals with the transmittedversion of the transmitted signal with the same code. The set of Nuniquely-coded signals are also received by a platform. The set of Nuniquely-coded signals are received absent reflection from thenon-cooperative object or target. The platform self-determines itsposition, motion, and orientation in the same coordinate system that theSDA of antenna arrays or signal subsystem used to determine the positionand motion of the non-cooperative object. Since the SDA of antennaarrays determines the position and motion of the non-cooperative objectand the platform separately self-determines a position, motion andorientation in a common coordinate system, jink maneuvers required byconventional systems for coordinate frame alignment are avoided.Consequently, the improved arrangement provides a savings in guidancesystem resources and reduces time delays in such navigation or guidancesystems. In addition, because the SDA of antenna arrays is tracking thetarget in the same coordinate frame that the platform isself-determining its own position and motion, no frame alignment isrequired, which also saves guidance system resources and reduces timedelays.

As indicated, a set of uniquely identifiable signals and or unique codedsignals may comprise a set of signals where each member signal isseparately distinguishable from each of the remaining member signals.For example, separate electromagnetic radio-frequency ranges or channelsfrom about 20 MHz to just under 100 GHz can be used to identify a set ofseparately distinguishable signals. This technique is commonly known asfrequency-division multiplexing (FDM). FDM is an analog technology thatdivides a select frequency spectrum into logical channels. In thecontext of this application, each of the separate spatially-distributedantenna arrays is used to transmit a respective signal or channel. Dueto the unpredictable Doppler shift of the signal spectrum in mobileenvironments, the channels are separated by guard bands that include arange of frequencies that lie between adjacent channels. None of thespatially-distributed antenna arrays is configured to purposely transmitsignals in the guard bands. One or more radio-frequency filters may bedeployed in support electronics to reduce interference in the channelsand guard bands as may be desired. While the guard bands reduce theprobability that adjacent channels will interfere, they decrease theutilization of the frequency spectrum.

As is known, various ranges of radio frequencies or bands are betterthan others for specific radar applications. For example, for relativelylower frequency signals it is easier to generate relatively greatertransmit signal power. In addition, relatively lower frequency signalsrequire larger antennas to determine angles accurately and are lesssusceptible to signal attenuation due to environmental conditions.Conversely, for relatively higher frequency signals it is more difficultto generate significant transmit power and there is greater attenuationof transmit signal power. However, relatively higher frequency signalscan take advantage of relatively smaller antennas and also providerelatively better accuracy and angular resolution of receivedreflections. Those skilled in the art of developing radar systemsunderstand the trade-offs with the application of various frequencybands.

As is known, one or more oscillating signals having the same frequencycan be shifted in degrees or time with respect to an unmodified memberof the set of signals to generate respective phase differences betweenthe oscillating signals. The phase difference between a reference orunmodified oscillator and time-shifted oscillators at the same frequencycan be expressed in degrees from 0° to 360° or in radians from 0 to 2π.In the context of this application, one of the spatially-distributedantenna arrays is provided a signal from a reference oscillator and eachof the remaining antenna arrays is provided a time/phase delayed versionof the reference oscillator to generate a set of respective phaseseparated signals.

One method to generate phase separated signals is by using LinearFrequency Modulation (LFM) or Non-Linear Frequency Modulation (NLFM) togenerate the unique signals. For LFM the frequency is increased(Up-chirp) or decreased (Down-chirp) in a linear fashion over the pulsethus creating a distinctive phase relationship. The Up-chirp signal canbe separated from the Down-chirp signal by bandpass filtering the matchfilter outputs. The degree of separation is a function of the linearfrequency slope and the time duration of the pulse commonly referred toas the time-bandwidth (TB) product. The higher the TB product the moreseparation is achieved. A similar separation can be achieved with NLFMsignals using the TB product.

Costas codes are another example of using frequency changes to modulatethe phase. In this case the pulse is divided into several smaller pulsesand the frequency for each pulse is determined based on a schedule offrequencies that optimize signal separation performance. The finitenature of the Costas coding schemes requires large code length toachieve moderate signal separation.

Time-division multiplexing is another signal processing technique thatcan be applied to both digital and analog signals to logically separatetransmitted signals from one another. A system architect defines a setof time slots that are respectively assigned to each of thespatially-distributed antenna arrays. In the context of thisapplication, a specific spatially-distributed antenna array is assignedto transmit a corresponding signal within a designated time slot.Time-division multiplexing operates in a synchronized fashion at boththe transmit node (i.e., an antenna array) and receiving nodes (a remoteplatform or other remote receiver). That is, when a first antenna arrayis transmitting a receiver functioning in synchronization with thetransmitter “understands” that it is receiving information from thefirst antenna array and not from any of the remaining antenna arrays.Persons skilled in the art of radio-frequency communications arefamiliar with the use of oscillating circuits and control systems togenerate both stable transmit frequencies and precisely timed clocksignals. For example, a phase-locked loop circuit generates an outputsignal that is related to the phase of an input signal. Phase-lockedloops can keep input and output frequencies the same over a range ofoperating conditions and can be used to synchronize signals identifyingtime slots in a time-division based signaling scheme.

As indicated, time differentiated communication systems must carefullysynchronize the transmission times from each of the spatiallydistributed antenna arrays to ensure that they are received in thecorrect time slot and are distinguishable from each other. Since suchsynchronization cannot be perfectly controlled in a mobile environment,each time slot may be arranged with adjacent guard slots that reduce theprobability that signals from respective antenna arrays will interfere,but at the expense of spectral efficiency.

Code-division multiplexing is another signal processing technique thatcan be applied to logically separate transmitted signals from oneanother. A communication system architect defines a set of uniqueorthogonal codes in a one to one relationship with each of thespatially-distributed antenna arrays. Each remote platform receiver or aremote receiver knows in advance which of the unique orthogonal codeshas been assigned to a particular spatially-distributed antenna array.Since it is not possible to create unique sequences that are orthogonalfor random starting points and which can make use of a code space,unique “pseudo-random” or “pseudo-noise” (PN) sequences are used inasynchronous code-division communication systems. PN sequences arebinary signals that appear to be random but can be reproduced byintended receivers.

Gold codes are an example of a PN sequence suitable for use in mobilecommunication systems where a specific antenna array can be assigned aunique code or signature. A particular Gold code is used to modulate thetransmit signal from a particular member of the antenna array. Suchsequences have bounded and small cross-correlations across a set.Alternatively, Kasami codes (a particular type of Gold code) can replacethe Gold codes or in particularly noisy channels Hadamard codes orWalsh-Hadamard codes can be deployed. Another known alternative includesthe application of complex-valued sequences, which when applied to radiosignals generates a signal having a constant amplitude, wherebycyclically shifted versions of the sequence result in zero correlationat a remote receiver. Such sequences are commonly known as Zadoff-Chusequences. The cyclically shifted versions of these sequences areorthogonal to one another, provided that each cyclic shift, when viewedwithin the time domain of the signal, is greater than the combinedpropagation delay and multi-path delay-spread of that signal between thetransmitter and receiver.

In addition to the aforementioned time, frequency andphase-differentiated communication signaling techniques for uniquelyidentifying a particular signal from a set of received signals, antennapolarizations can be manipulated or adjusted as well. An antennapolarization is defined by the orientation of the electric field orE-plane of the radio wave with respect to a common reference plane(e.g., the Earth's surface). An antenna's polarization is determined byits physical structure and orientation. In general, an antenna'spolarization is elliptical. In some cases, the ellipse collapses andappears as a line (i.e., linear polarization). In linear polarization,the electric field of the radio wave oscillates in a single directionperpendicular to the direction of propagation of the radio wave. Inother arrangements, the two axes of the ellipse are equal and produce acircular polarization. In circular polarization arrangements, both theelectric field and the magnetic field rotate about an axis ofpropagation Polarized elliptical or circular radio waves are designatedas right-handed for counter-clockwise rotation about the axis ofpropagation or left-handed for clockwise rotation about the axis ofpropagation.

For many radar applications the transmit antenna polarization is chosento be either vertical (E-plane) or horizontal (H-plane). For avertically polarized (Co-pol) antenna the separation of horizontallypolarized (Cross-pol) signals is determined by the isolation of theantenna or the relative power difference between Co-pol signals andCross-pol signals. Thus, when one antenna is transmitting and receivingvertically polarized signals and another is transmitting and receivinghorizontally polarized signals the signal separation is determined bythe degree of isolation provided by the receive antennas. Othercombinations of antenna polarizations that can provide separation areleft-hand circular and right-hand circular.

In an example embodiment, the platform uses one or more of aself-determined position, motion and orientation of the platform and oneor more of a received position, motion and orientation of thenon-cooperative object, as communicated by the SDA of antenna arrays, toguide or navigate the platform relative to the non-cooperative object.Such guidance of the platform relative to the non-cooperative object canadapt to present circumstances of the platform and the non-cooperativeobject in accordance with an operational mode of the platform. Forexample, in some embodiments the platform may operate in an interceptmode where a collision or near collision between the platform and anon-cooperative object are intended. Whereas, in other operational modesthe platform is intended to avoid a non-cooperative object. Whenfunctioning in these alternative operational modes the platform may beprogrammed to orbit a non-cooperative object or maintain a desired rangeof separation distances and angles with respect to a non-cooperativeobject.

In an alternative embodiment a platform is arranged with a thirdreceiver that receives reflections of the uniquely coded signalsreflected by the non-cooperative object. In this example, the platformreceives the reflected versions of the uniquely coded signals with thethird receiver and generates a self-determined position (of theplatform) and a platform determined position of the non-cooperativeobject to guide the platform with respect to the non-cooperative objectin the coordinate system.

Example platforms that may use a self-determined position and a receivedposition of a non-cooperative object in a common coordinate systeminclude land-based vehicles and ships or other craft on the surface of abody of water. Other example platforms may include a portable devicethat is temporarily attached to an article of clothing worn by a person.These example platforms can use embodiments of the disclosed systems intwo dimensions or three dimensions. Example non-cooperative objects thata platform may intercept or avoid include other land-based vehicles,ships or other watercraft, natural items and man-made structures.

Other example platforms that may use a self-determined position and areceived position of a non-cooperative object in a common coordinatesystem include, for example, a missile, projectile, aircraft andspacecraft. These example platforms are more likely to use embodimentsof the disclosed systems that operate in three dimensions. Thesenon-terrestrial platforms may be guided with respect to non-cooperativeobjects that are both terrestrial and non-terrestrial. For example,non-cooperative objects in these embodiments may include land-basedvehicles, ships or other watercraft, natural items, man-made structures,missiles, projectiles, aircraft and spacecraft.

An example embodiment of a navigation system can take advantage of theself-determined position, motion, and orientation of a platform in thecoordinate system defined by the SDA of antenna arrays. For example, anavigation system can be arranged to assist ships as they navigate in ornear a harbor. In such an embodiment, a SDA of antenna arrays transmitsthe uniquely coded signals directly to each ship arranged with acompatible receiver. A ship arranged with a compatible receiver (e.g., aplatform) can self-determine a position or location in the coordinatesystem defined by the SDA of antenna arrays. The ship will also receiveone or more signals describing the position and motion (if any) of oneor more non-cooperative objects or features in the harbor in the samecoordinate system.

In some alternative embodiments, the ship can transmit a signalincluding one or more identifiers and its self-determined position orlocation to other ships in the harbor. Or a transponder could beoutfitted on each ship or buoy that would receive and retransmit theuniquely coded signals to a second receiver on the ship that wouldprocess the signals to determine the location of the ships or buoys inthe SDA coordinate frame. In this case a common clock will be requiredfor each ship or platform to determine the range or distance from theSDA to each ship-based receiver. The transponder can be configured toapply a fixed frequency shift to the received uniquely coded signals forenhanced detection in sea clutter and for identification of thetransponder platform.

Also, the ship may receive a list of known ship or buoy locations in thecoordinate system defined by the SDA of antenna arrays from a receiversubsystem in communication with and at a known position relative to theorigin defined by the SDA. The list may be provided in a configurationfile and stored in a memory element accessible to a processor incommunication with the compatible receiver. The list may be provided andstored well before the ship arrives at the entrance to the harbor.Otherwise, the list may be communicated in a signal dedicated for thatpurpose that is broadcast near the entrance of a harbor. In addition tothe ship and buoy locations, the configuration file or local informationmay further include a set of way points defining a preferred channel orpath for ships entering or exiting the harbor. The described navigationsystem may use a SDA of antenna arrays that define a two-axis coordinatesystem that compatible receivers can use to describe position, motionand orientation of ships and buoys in the harbor.

In this regard, the improved navigation or guidance systems may bearranged to communicate with cooperative objects in the environment thatare outfitted with a suitable transponder. These cooperativetransponders receive the N uniquely coded signals and modify the samebefore transmitting a modified version of the N uniquely coded signalstoward a receiver subsystem or a platform or platforms in theenvironment. Such a device can be arranged to receive, modify, amplifyand transmit modified versions of the N uniquely coded signals with aminimal delay. When modified by shifting the frequency by a uniquevalue, the transponder may uniquely identify a cooperative platform suchas a ship (which may or may not be moving) or a buoy that is fixed in aharbor. A transponder deployed on a ship could use a frequency shift oradjustment that is significantly greater than that which could beexpected from any Doppler shift as a result of a moving surface ship.Furthermore, a suitably arranged transponder on a buoy would enhance theprobability of a positive identification during adverse weather and/orhigh seas.

Similarly, an example embodiment of a navigation system can be arrangedto assist planes as they navigate between hangars along a tarmac or evenon taxiways and runways of an airport. In such an environment, a SDA ofantenna arrays transmits the uniquely coded signals. A plane arrangedwith a compatible receiver (e.g., a movable platform) can self-determinea position or location in the coordinate system defined by the SDA ofantenna arrays. In addition, the plane receives one or more signalsindicative of the position and motion (if any) of non-cooperativeobjects, landmarks, or obstacles in the common coordinate system definedby the SDA of antenna arrays.

In an alternative embodiment, the aircraft can transmit a signalincluding one or more identifiers and its self-determined position orlocation to other aircraft at the airport and an optional groundcontroller. The aircraft may receive a data file or list describingrunways, taxiways, outdoor temporary parking locations, hangars, etc. ata particular airport in the coordinate system defined by a local SDA ofantenna arrays. The data file, database or list including localinformation may be provided and stored in a memory element accessible toa processor in communication with the compatible receiver. The airportspecific local information may be provided and stored well before theaircraft arrives at the airport. Otherwise, the airport specificinformation may be communicated in a signal dedicated for that purposethat is broadcast as aircraft enter a controlled airspace near theairport. In addition, the above described data may further include a setof way points defining a preferred course or path for aircraft to usewhile taxiing from a runway to a particular hangar, gate, refuelingstation or other select destination at the airport. The describednavigation system may use a SDA of antenna arrays that define a two-axiscoordinate system that compatible receivers can use to describeposition, motion and orientation of aircraft on the ground at theairport.

Another alternative embodiment of a navigation system can be arranged todirect public safety personnel in a building or other structure in theevent of an emergency. In this embodiment, a SDA of antenna arraystransmits the uniquely coded signals. A fireman or police officer may beprovided a portable device or receiver that can be clipped or otherwisesecured to a belt or article of clothing worn by the individual. Theportable receiver (e.g., a platform) can self-determine a position orlocation in the coordinate system defined by the SDA of antenna arrays.In addition, the portable receiver receives one or more signalsindicative of the position and motion (if any) of non-cooperativeobjects, landmarks, or obstacles in the common coordinate system definedby the SDA of antenna arrays.

In an alternative embodiment, the portable receiver may be arranged witha speaker or other output device to provide audible tones or commands toassist the wearer of the portable receiver. In addition, an on-sitecontroller may be provided to coordinate the actions of multiple safetypersonnel.

In an example embodiment, the portable receiver can transmit a signalincluding one or more device identifiers and its self-determinedposition or location to other personnel and an optional emergencycoordinator or control entity. The portable receiver may be pre-loadedwith a map or floorplan describing the layout of locations within thebuilding. Such layout or local information may include the location ofhallways, rooms, cubicles, mechanical rooms, elevators, stairways, etc.for a particular floor of the building in the coordinate system definedby the SDA of antenna arrays. In addition, the above described localinformation may further include a set of way points defining a preferredcourse or path to exit the building. The described navigation system mayuse a SDA of antenna arrays that define a two-axis coordinate systemthat compatible receivers can use to describe position, motion andorientation of the portable receiver in a coordinate system defined bythe SDA of antenna arrays.

In still another example embodiment, additional platforms are arrangedwith respective second and third receivers. When used in this context, areceiver is a device or collection of elements that converts anover-the-air signal into one or more items of useful information. Atleast a first member of a group of platforms determines its respectivedistance from the non-cooperative object. At least two additionalmembers of the group of platforms communicate a respective presentposition and a respective distance to the non-cooperative object in thecoordinate system defined by the SDA. With this information, the firstmember of the group of platforms determines a position of thenon-cooperative object in the coordinate system. The first member of thegroup of platforms communicates the position of the non-cooperativeobject to one or more of the remaining members of the group of platformsin the common coordinate frame defined by the SDA thereby allowing eachplatform to implement autonomous guidance relative to thenon-cooperative object.

Alternatively, the first member of the group of platforms uses one ormore of the position, motion and orientation of the first member of thegroup of platforms and one or more of the present position, motion andorientation of the non-cooperative object to generate a guidancesolution to direct the first member of the group of platforms relativeto the non-cooperative object. The first member of the groupcommunicates its position, motion, and orientation to one or more of theremaining members of the group of platforms in the common coordinateframe defined by the SDA of antenna arrays. Since the platformsself-determine their position, motion, and orientation in the commonframe defined by the SDA of antenna arrays, the remaining members of thegroup of platforms (i.e., those members other than the first member) maydetermine a respective separation distance and relative direction withrespect to the first member of the group of platforms for the entiregroup of platforms to controllably navigate with respect to thenon-cooperative object.

In another example embodiment, a platform includes a third receiver thatreceives a signal from a source other than the uniquely coded signalsthat are reflected from the non-cooperative object and other than acooperative object that transmits a modified version of the N uniquelycoded signals. In this example, the platform processor uses informationfrom the signal received by the third receiver to determine a positionof the non-cooperative object in a second coordinate system differentfrom the coordinate system defined by the SDA of antenna arrays.However, the transformation from the second coordinate system to thecommon system defined by the SDA of antenna arrays must be made known tothe platform.

In still another example embodiment, additional platforms are arrangedwith respective second and third receivers as well as a transmitter andrelated circuitry for generating a new code that uniquely identifies aplatform. The transmitter connected to or otherwise supported by thecorresponding platform is used to generate and propagate aradio-frequency signal modulated with the respective new code, which isdifferent from the codes transmitted from the SDA of antenna arraysdefining the first coordinate system. In this embodiment, a platform ora group of proximally located platforms that are self-locating in thecoordinate frame defined by the SDA of antenna arrays define orestablish a new coordinate frame. The origin of the new coordinate framecan be established as the location of an identified platform or as afunction of the locations of two or more platforms as determined withrespect to the first coordinate system as defined by the SDA of antennaarrays. A swarm or set of proximally located platforms may be able totake advantage of the finer resolution that may be possible in theextended or new coordinate system.

In this alternative embodiment, at least a first member of a group ofplatforms determines its respective distance from the non-cooperativeobject. This determination can be made in the first coordinate framebased on reflected versions and directly received versions of thesignals from the SDA of antenna arrays alone. The range to thenon-cooperative object may be confirmed, replaced or adjusted based onround trip times of a uniquely coded signal transmitted from theplatform, reflected by the non-cooperative object and received by theplatform. One or more proximally located platforms may shareself-determined location information derived in the first coordinatesystem and may add a confirmed, replaced, or adjusted range to thenon-cooperative object based on respective round-trip times of arespective uniquely coded signal transmitted from the respectiveplatform. One or more of the proximally generated platforms may use therespective locations of the platforms and the respective ranges to thenon-cooperative object to generated guidance and or navigation solutionswith respect to the non-cooperative object. These guidance and ornavigation solutions may be determined in the new coordinate frame andshared across the set of proximally located platforms.

In still another embodiment, a group of platforms can be configured toinclude a pilot platform, a set of forward-based platforms, and one ormore interceptor platforms. The pilot platform is configured with a SDAof antenna arrays that are transmitting respective uniquely identifiablesignals and a first or pilot receiver. The uniquely identifiable signalstransmitted from each of the respective antenna arrays can be steered ordirected as desired to increase the likelihood that the signals arereflected to the pilot platform receiver. As in other arrangements, therelative position of the pilot platform receiver with respect to anorigin defined by the spatially-distributed antenna arrays is known.Additionally, as in the other arrangements the pilot platform is furtherconfigured with one or more signal generators and signal processorsarranged to generate, distribute and control the transmission of theuniquely-identifiable signals and to receive and derive informationabout the locations, motion and orientation of the forward-basedplatform(s) and the one or more interceptor platforms from informationderived from reflected versions of the uniquely identified signals.

Alternatively, the pilot platform may be arranged to transmit uniquelycoded signals from the SDA of antenna arrays. As described, differencesin time of arrival and phase of the uniquely coded signals as receivedby a forward-based or remote platform can be used by a platformprocessor to self-determine a relative location in a coordinate systemdefined by the arrangement of the SDA of antenna arrays. In addition tothe uniquely coded signals, the pilot platform may be arranged toperiodically transmit an information signal that identifies a presentposition of the pilot platform.

The pilot platform may be arranged with a cargo hold or other support tocontain or carry the forward-based platform and one or more interceptorplatforms until the group of platforms is proximal to a defined locationrelative to a target or non-cooperative object. Upon arrival of thegroup of platforms at such a defined location, the forward-basedplatform(s) and one or more interceptor platforms may be energized anddeployed. Alternatively, the group of platforms may be separatelydelivered or deployed by other vehicles or methods or may be configuredto autonomously rendezvous at a designated location as may be desired.

The forward-based or remote platform is arranged with a receiver, aninertial navigation system and a sensor in addition to one or morecontrol systems. The sensor may be an active sensor, a passive sensor,or may have operational modes where the sensor alternates between activeand passive modes of operation. In some arrangements, a forward-based orremote platform may be arranged with a synthetic aperture radar system,one or more antennas and transceivers for intercepting IR and other NCOgenerated RF signals.

Radar, sonar, or optical sensors (including infrared sensitive devices)are envisioned. Such sensors include associated electronics foramplifying and perhaps filtering incident light or sound received by oneor more photosensitive diodes, transducers, or in the case of radar, forcapturing electromagnetic energy from specific wavelengths andconverting the same to electric signals before processing the same. Oneor more optical elements may be arranged to intercept, reflect and orcollimate incident light. In some arrangements such sensors may relyentirely on reflected light from a remote source. Alternatively, suchsensors or sensor systems may include support electronics and one ormore light emitters and various optical elements for collimating andotherwise directing an active light source. Such sensors, howeverembodied, may be arranged with a field of view that is likely toencounter reflected energy from a non-cooperative object or target ofinterest. When a relatively narrow field of view is provided by suchsensor systems, the optical elements and perhaps the photosensitivearrays of elements may be arranged in a gimbal with a correspondingcontrol system arranged to track the reflected beam of electromagneticenergy.

Whether such optical sensors are passive or active, angular resolutionof a beam vector together with information from the inertial navigationsystem can be used to determine a target location with respect to theforward-based or remote platform. The forward-based platform can bearranged with one or more transceivers and antennas to communicate oneor more informational signals including the location, orientation andmotion (if any) of the platform and/or a non-cooperative object ortarget. The one or more informational signals may be communicated to oneor more interceptor platforms within range of the forward-basedplatform.

In some arrangements, the forward-based platform can be arranged withone or more propulsion systems to controllably navigate autonomouslyabout a target. In addition, the forward-based platform may useinformation from the sensor in addition to information from the inertialnavigation system to navigate or guide the forward-based platformrelative to a desired position or location proximal to a target or tonavigate or guide the forward-based platform relative to the target ornon-cooperative object without such an offset. Accordingly, theforward-based platform may be programmed to orbit or traverse a desiredpattern.

The one or more interceptor platforms are configured with a respectivereceiver, inertial navigation sensor, interceptor processor and one ormore respective control systems. In some arrangements, a select one ormore of the interceptor platforms can be arranged with one or moreoptional propulsion systems to controllably navigate the interceptorplatform with respect to a target or other designated location ascommunicated from the pilot platform. However delivered or deployed, theone or more interceptor platforms are arranged to self-determine arespective position relative to the pilot platform. Each of the one ormore interceptor platforms is arranged to use one or both of theself-determined position as determined by the uniquely identifiedsignals and/or the interceptor specific inertial navigation sensor and atarget location as communicated periodically from the pilot platform todetermine a guidance solution that will intercept the target ornon-cooperative object.

When the forward-based platform and one or more interceptor platformsare deployed from a pilot platform, the respective inertial navigationsystem may be initially set or otherwise configured to identify a sharedposition or location with the pilot platform soon after the variousplatforms are energized. However, inertial navigation systems oftenintroduce errors that may accumulate over time such that the estimatedposition of the forward-based platform and one or more interceptorplatforms may drift or stray from a desired position and orientation. Incases where the inertial navigation systems are not calibrated oradjusted with respect to the coordinate system defined by thespatially-distributed antenna arrays on the pilot platform, a set ofcorrective signals may be required to accurately coordinate the variousplatforms. To maintain accuracy, the forward-based platform'sself-determined position is periodically or intermittently aligned oradjusted with information determined on the pilot platform.

In this regard, the forward-based platform determines its position andvelocity in a second coordinate frame or coordinate system determined bythe inertial navigation sensor and communicates both its velocity vectorand time and phase measurements to the pilot platform. The pilotplatform uses the time and phase measurements to estimate theforward-based platform position and velocity in the first coordinateframe or coordinate system defined by the spatially-distributed antennaarrays and then determines a coordinate transform that aligns theforward-based platform determined velocity vector with the pilotplatform estimate of the forward-based platform velocity vector toestablish a frame alignment. The forward-based platform also determinesthe location of a non-cooperative object in the second coordinate frameand communicates the location to the pilot platform. The pilot platformeither directly or indirectly communicates the location of thenon-cooperative object in the first coordinate frame to the interceptorplatforms allowing these platforms to guide to the non-cooperativeobject location.

In another alternative embodiment, a set of one or more interceptorplatforms is provided. A surface-based group of spatially-distributedantenna arrays are arranged to transmit respective uniquely identifiablesignals. A receiver system is co-located with the group ofspatially-distributed antenna arrays or in a known location with respectto the spatially-distributed antenna arrays. The uniquely identifiablesignals transmitted from each of the respective antenna arrays can besteered or directed as desired to increase the likelihood that thesignals are reflected by the one or more interceptor platforms to thepilot platform receiver. As in other arrangements, the relative positionof the pilot platform receiver with respect to an origin defined by thespatially-distributed antenna arrays is known. Additionally, as in theother arrangements the pilot platform is further configured with one ormore signal generators and signal processors arranged to generate,distribute and control the transmission of the uniquely-identifiablesignals and to receive and derive information about the locations,motion and orientation of the one or more interceptor platforms frominformation derived from reflected versions of the uniquely identifiedsignals.

In this alternative embodiment, the one or more interceptor platformsare arranged with respective transceivers, platform processors, signalgenerators, and first and second platform antennas. In contrast with theprevious embodiment that used a forward-based platform with a sensor orsensor system to identify and locate a position of a target ornon-cooperative object, the one or more interceptor platforms generateand transmit a second set of platform unique signals that are directedtoward a target or non-cooperative object of interest. Reflectedversions of the set of platform unique signals are received at therespective interceptor platforms and processed by the respective one ormore interceptor processors. Accordingly, in such an arrangement each ofthe one or more interceptor platforms are arranged to self-determine aposition in a coordinate system defined by the spatially-distributedantenna arrays, as well as determine an angular rotation and range whichcan be used to determine a position of a target or non-cooperativetarget with respect to interceptor platform. A respective processor canuse this information to determine an appropriate guidance or navigationsolution to apply to an interceptor platform-based control system or tocommunicate a position of the target to a surface-based control entityoperating the spatially-distributed antenna arrays.

In the figures, like reference numerals refer to like parts throughoutthe various views unless otherwise indicated. For reference numeralswith letter character designations such as “102a” or “102b”, the lettercharacter designations may differentiate two like parts or elementspresent in the same figure. Letter character designations for referencenumerals may be omitted when it is intended that a reference numeralencompass all parts having the same reference numeral in all figures.

An environment 100 in which an example embodiment of an improvedtracking and/or guidance system operates is illustrated in FIG. 1. Theimproved tracking and/or guidance system includes aspatially-distributed architecture (SDA) or signal generation sub-system110 that is separated or remotely located from a non-cooperative objector target 120. In the illustrated embodiment, the SDA 110 is arranged orlocated to the same side of each of the non-cooperative object or target120, a cooperative object 122, a receiver subsystem or first receiver130, a platform 150, as well as an alternative signal source 180. TheSDA 110, receiver subsystem 130 and platform 150 are not so limited andin modified environments the SDA 110 will be spatially located in otherrelationships with respect to the receiver subsystem 130, platform 150,non-cooperative object or target 120, cooperative object 122 and thealternative signal source 180.

As indicated schematically in FIG. 1, the SDA 110 defines a firstcoordinate system 5. The first coordinate system 5 includes an origin 10where an X-axis 12, a Y-axis 13, and a Z-axis 14 meet. As furtherindicated schematically in FIG. 1, the X-axis 12 is orthogonal orapproximately orthogonal to both of the Y-axis 13 and the Z-axis 14. Inaddition, the Y-axis 13 is orthogonal or approximately orthogonal to theZ-axis 14. The first coordinate system 5 provides a mechanism tospatially define the relative location and orientation of items in theenvironment 100. While the origin 10 may be defined at any locationwithin or about the SDA 110, the origin 10 is preferably located at thephase center of the N antenna arrays forming the SDA 110.

In the illustrated embodiment a three-dimensional coordinate space isshown. However, it should be understood that under some circumstances(e.g., operation of a motorized vehicle such as a radio-controlled car,a surface ship, a taxiing aircraft or a car over surfaces where there islittle, if any change in one of the orthogonal dimensions) atwo-dimensional coordinate space or X-Y plane is still useful forlocating or defining a position of a portable device, the surface ship,taxiing aircraft, car or any other signal reflecting item on or near theX-Y plane. The location of non-signal reflective items may becommunicated via local information describing an environment 100. As iswell known, a position or point on the X-Y plane is identified by twoperpendicular lines that intersect each other at the point, which isdefined by X-Y coordinates each separately defined by a signed distancefrom the origin to the respective perpendicular line. Alternatively,each point on a plane can be defined by a polar coordinate system wherea point is defined by a distance from a reference point or origin and anangle from a reference direction.

In three dimensions, three perpendicular planes (e.g., a X-Y plane, aY-Z plane, and a X-Z plane) that intersect each other at an origin areidentified and three coordinates of a position or point in thethree-dimensional coordinate space are defined by respective signeddistances from the point to each of the planes (e.g., point x, y, z).The direction and order for the respective three coordinate axes definea right-hand or a left-hand coordinate system. The first coordinatesystem 5 is a right-hand coordinate system. Alternative coordinatesystems can replace the first coordinate system 5. Such alternativesinclude a cylindrical coordinate system or a spherical coordinatesystem.

Wherever located in the environment 100 with respect to the receiversubsystem 130, the platform 150, the non-cooperative object 120,cooperative object 122 and the alternative or optional signal source180, the SDA 110 generates and controllably transmits N uniquely codedsignals 113 where N is a positive integer greater than or equal to two.The SDA or signal generation subsystem 110 includes at least one signalgenerator 111 and N antenna arrays 112. As indicated in FIG. 1, the Nuniquely coded signals 113, generated by and transmitted from the SDA110, impinge or directly encounter both the non-cooperative object 120and the platform 150. These non-reflected versions of the N uniquelycoded signals 113 are reflected by one or more surfaces of thenon-cooperative object or target 120 such that R reflections 114 of theN uniquely coded signals 113 are received by one or more antennas 132 atthe first receiver or receiver subsystem 130.

The improved systems and methods for guidance or navigation may bearranged to consider various objects as non-cooperative objects 120 inaccordance with an environment of interest. For example, if the systemis deployed in a harbor a group of non-cooperative objects 120 mayinclude surface ships and other watercraft, buoys, flotsam, jetsam, etc.By way of further example, when the system is arranged to guide airborneplatforms a group of non-cooperative objects 120 may include missiles,projectiles, aircraft, and even spacecraft. In still other examples, anon-cooperative object 120 may include stationary or non-stationaryobjects supported by land such as, cars, trucks, trains, tanks, fences,buildings, etc. It should be understood that when one or morecooperative objects 122 a-122 n are present in the environment 100 thesecooperative objects 122 a-122 n may also reflect the N uniquely codedsignals 113. Cooperative objects 122 may include any stationary ornon-stationary object whether on land, on the surface of a body ofwater, or airborne that communicates in some way to one of the receiversubsystem, the SDA or the one or more platforms 150.

In the illustrated embodiment, the tracking and/or guidance system 100includes a receiver subsystem 130 and a platform 150. The SDA 110 may bea fixed station on the ground or a moving station disposed on a movingplatform such as, for example, a ship, an airplane, a flying drone, atruck, a tank, or any other type of suitable vehicle (not shown). TheSDA 110 includes an array of N antenna elements 112, a signal generator(SG) 111 and other elements (not shown in FIG. 1). The SDA 110 can becollocated with the receiver subsystem 130, or as shown in theillustrated embodiment, is removed from but at a known position in thefirst coordinate system 5 relative to the origin 10. Together, the SDA110 and the receiver subsystem 130 determine a position of the target ornon-cooperative object 120 in the coordinate system 5. The receiversubsystem 130 is arranged with a radio-frequency communication link tosend wireless information signals 140 to the SDA 110. One or more clocksignals, synchronization signals or codes may be communicated from theSDA 110 to the receiver subsystem 130 over the radio frequencycommunication link. Alternatively, the receiver subsystem 130 uses oneor more wired connections to send information signals 139 to the SDA110. In an alternative arrangement, the above described clock signals,synchronization signals or codes are communicated via wired connectionsfrom the SDA 110 to the receiver subsystem 130. However arranged, theinformation signals 139 or the wireless information signals 140 includeinformation responsive to one or more characteristics of the R reflectedversions 114 of the N uniquely coded transmit signals 113, where R and Nare positive integers and where R is less than or equal to N.

When so desired, the radio-frequency communication link may be arrangedto send additional wireless information signals to one or morecooperative objects 122 a-122 n. These wireless information signals mayinclude local information such as a floor plan, a harbor chart, anairport map, a city map, etc. In addition, the wireless informationsignals may include transponder configuration parameters. For example, atransponder configuration parameter may include a fixed frequencydifference that a particular transponder is directed to apply to the Nuniquely coded signals 113 received by the transponder. Each transponderin the environment 100 will be associated with one of the cooperativeobjects 122 a-122 n. Otherwise, the transponders associated with therespective cooperative objects 122 may include firmware or storedinformation that may include local information and a respectivemodification for the transponder to apply to the received N uniquelycoded signals 113 before transmitting modified versions 117 of the Nuniquely coded signals. In operation, modified versions 117 of the Nuniquely coded signals 113 transmitted from the respective transpondersin accordance with a designated modification can be used by one or moreplatforms 150 to identify the location and motion (if any) of therespective cooperative objects 122 in the coordinate system 5. Examplemodifications to the uniquely coded signals 113 may include one or moreof changes in frequency, time, phase or polarization. A separatelyidentifiable change in any of these parameters or in combinations ofthese parameters can be used to uniquely identify cooperative objects122 a-122 n in the environment 100.

In the example embodiment, the receiver subsystem 130 is arranged withprocessing circuitry or a processor 131, memory 135, signal generator138 and one or more antennas 132. The memory 135 includes one or morelogic modules and data values (not shown) that when controllablyretrieved and executed by the processor 131 enable the processor 131, inresponse to information derived from the R reflections 114 of the Nuniquely coded signals 113 received at the antenna 132, to determine aposition of the non-cooperative object 120 in the first coordinatesystem 5. Changes in the location of the non-cooperative object 120relative to the SD architecture 110 and/or the receiver subsystem 130may also be determined by the processor 131. In turn, the processor 131forwards the location and motion information associated with thenon-cooperative object 120 to the signal generator 138 to format,amplify and or buffer the information for communication to the SDarchitecture 110 via one or both of the communication link 139 and thecommunication link 140

In addition, the receiver subsystem 130 can be arranged with one or moreantennas and one or more transceivers or one or more transducers orphotosensitive semiconductors in any desired number or physicalrelationships to receive one or more signals responsive to thenon-cooperative object 120. The one or more signals, which are separateand distinct from the N uniquely coded signals 113 or the R reflectedversions of the N uniquely coded signals 114, may originate at the NCO(e.g., when the NCO is actively transmitting RF signals, creating one ormore identifiable sounds or when the NCO is generating heat.)Alternatively, the one or more signals may include reflected versions ofsignals that originate from a receiver subsystem arranged to generatesuch signals or other signal sources capable of transmitting signalsthat intersect one or more surfaces of the non-cooperative object 120.If the receiver subsystem 130 receives only these one or more signalsseparate and distinct from the reflected versions of the N uniquelycoded signals, the receiver subsystem 130 or the SD architecture 110will transform or convert the NCO location to the coordinate frame 5before forwarding the NCO location to one or more of the platforms 150a-150 n or before forwarding the NCO location to one or more cooperativeobjects 122 a-122 n.

One or more of the N antenna arrays 112 or a separate dedicated antenna(not shown) is provided to wirelessly communicate information regardingthe location and motion (if any) of the non-cooperative object or target120 via communication link 115 to the platform 150. The platform 150uses the location and motion information received from the SDA 110 totrack the location of the non-cooperative object 120. In addition, theplatform 150 uses both the location and motion information received fromthe SDA 110 and a self-determined location and motion as inputs to guideor navigate the platform 150 with respect to the non-cooperative object120. Thus, the platform 150 can be programmed or configured to operatein various modes of operation. For example, when the non-cooperativeobject 120 is in motion, the platform 150 can be configured to operatein a track mode where movements of the non-cooperative object 120 arerecorded by the platform 150. By way of further example, the platform150 can be configured to track and maintain a specified separationdistance from the non-cooperative object or target 120. In anotherexample, when the non-cooperative object 120 is stationary, the platform150 can be configured to orbit or in some situations avoid thenon-cooperative object 120. When so desired, the platform 150 can beoperated in an intercept mode that guides or directs one or more controlsystems of a projectile, missile, ship, airplane, drone, land-basedvehicle, portable receiver etc., supporting the platform 150 tointercept the non-cooperative object or target 120. An interceptcondition occurs when the platform 150 moves within a desired distanceof or contacts the non-cooperative object 120.

The platform 150 uses the location and motion information received fromthe SDA 110 to track the location of the non-cooperative object 120.Furthermore, the platform 150 uses both the location and motioninformation received from the SDA 110 and a self-determined location andmotion as inputs to guide or navigate the platform 150 with respect tothe non-cooperative object 120. Moreover, the platform 150 uses modifiedversions 117 of the N uniquely coded signals 113 to also locate,identify and determine relative motion (if any) of one or morecooperative objects 122 a-122 n that might be located in the environment100. Thus, the platform 150 can be further programmed or configured toavoid and/or track both cooperative objects 122 a-122 n as well asnon-cooperative object 120.

In the example embodiment, the platform 150 is arranged with processingcircuitry or a processor 151, memory 155, and one or more antennas 152.Platform 150 may be fixed to one or more of a missile, a projectile, aship, an airplane, a flying drone, a truck, a tank, or any other type ofsuitable vehicle or even a relatively small portable device (not shown).When the platform 150 is coupled to or part of a projectile, theplatform 150 may be dropped, launched, expelled or otherwise separatedfrom a ship, airplane, drone, or land-based vehicle. The one or moreantennas 152 receive the N uniquely coded transmit signals 113transmitted by the SDA 110. The memory 155 includes one or more logicmodules and data values (not shown) that when controllably retrieved andexecuted by the processor 151 enable the processor 151, in response toinformation derived from the N uniquely coded signals 113 as received atthe antennas 152, to self-determine a position of the platform 150 inthe coordinate system 5. Changes in the location of the platform 150relative to the SDA 110 may also be determined by the processor 151. Inaddition, one or more of the antennas 152 or a dedicated antenna (notshown) may receive information identifying the location and motion (ifany) of the non-cooperative object 120 as communicated by the SDA 110via the communication link 115. Thus, the one or more logic modules andstored data values can be transferred to the processor 151 to enable anyone of the described or other operational modes.

As also illustrated in FIG. 1, an optional or alternative signal source180 (or a set of such signal sources) may communicate an informationsignal 185 to the platform 150. The information signal 185 may bereceived by one or more of the antennas 152 one or more of the optionalantennas 154 and or a dedicated antenna (not shown). In an exampleembodiment, the information signal 185 includes location, motion (ifany) and orientation of the non-cooperative object 120 in accordancewith a coordinate system other than the coordinate system 5. Forexample, the information signal 185 may include location as defined bylatitude, longitude (in degrees, minutes, seconds format or in decimalformat) and altitude in meters with respect to sea level as determinedby a global positioning system (GPS) receiver or a signal sourceresponsive to such a system. By way of further example, the platform 150may be arranged with a GPS receiver (not shown) and the informationsignals 185 may each include a specific pseudorandom code known to thereceiver, a time of transmission and the location of the satellitebroadcasting the respective signal. In still other examples, therespective information signal may be sent from an airborne platformarranged with a synthetic aperture array that has identified a structureor other non-cooperative object 120. However configured, when thelocation of the non-cooperative object 120 is provided to the platform150 in a coordinate system other than the coordinate system 5 aconversion operation will be necessary for the platform 150 to determineits distance to the non-cooperative object or target 120.

As also illustrated by way of dashed lines, the platform 150 may beaccompanied by one or more instances of separate platforms 150 a-150 n.When so provided, each member of the group of platforms 150 a-150 n isarranged with one or more positioning antennas 152 and one or moretracking antennas 154. As described, the positioning antennas 152receive the N uniquely coded signals 113 transmitted from the SDA 110and the tracking antennas 154 receive reflected versions 114 of the Nuniquely coded signals that are reflected by the non-cooperative object120. When so arranged, at least one of the platforms 150 includes arespective platform processor (not shown) that determines a distance tothe non-cooperative object 120. The platform 150 receives informationfrom at least two other members of the remaining platforms 150 a-150 n.The shared information includes the respective self-determined position,motion and orientation in the coordinate frame 5 and the determinedposition and motion (if any) of the non-cooperative object 120 in thecoordinate frame 5. The platform(s) 150 may be arranged with dedicatedtransceivers and signal processors (not shown) for communicating withthe remaining platforms 150 a-150 n.

In addition, the platform 150 communicates a self-determined position,motion and orientation and the calculated position of thenon-cooperative object 120 in the coordinate frame 5 to other members ofthe group of platforms. Furthermore, the platform 150 may be arranged togenerate a guidance or navigation solution to direct platform 150 withrespect to the non-cooperative object 120. Such guidance solutions mayinclude instructions that direct control systems on the platform 150 tofollow or intercept a moving non-cooperative object 120, or to orbit orintercept a stationary non-cooperative object 120. In some embodiments,such guidance or navigation solutions may generate control signals thatdirect the platform along an intended path, route or channel. In theseembodiments, the guidance or navigation solutions may be arranged orprogrammed to avoid various objects in the environment 100. Inembodiments where multiple platforms 150 a-150 n are deployed eachplatform 150 will separately determine a guidance solution. Moreover,information may be shared with other members of the group of platforms150 a-150 n. Such information may assist a platform 150 that is notreceiving reflected versions 114 of the uniquely coded signals 113 tocontinue in a direction or path towards the non-cooperative object ortarget 120 until such time that whatever was blocking the path of thereflected signals is no longer in the way.

When so arranged, at least one of the platforms 150 includes arespective platform processor (not shown) that determines a distance tothe non-cooperative object 120. The platform 150 receives informationfrom at least two other members of the remaining platforms 150 a-150 n.The shared information includes the respective self-determined position,motion and orientation in the coordinate frame 5 and the determinedposition and motion (if any) of the non-cooperative object 120 in thecoordinate frame 5. The platform(s) 150 may be arranged with dedicatedtransceivers and signal processors (not shown) for communicating withthe remaining platforms 150 a-150 n.

As further illustrated by way of dashed lines, the environment 100 mayinclude one or more cooperative objects 122 a-122 n. When so provided,one or more platforms 150 a-150 n arranged with one or more positioningantennas 152 and one or more tracking antennas 154 will receive the Nuniquely coded signals 113 transmitted from the SDA 110, the reflectedversions 114 of the N uniquely coded signals that are reflected from anon-cooperative object 120 and modified versions 117 of the N uniquelycoded signals 113 that are received, modified and transmitted from theone or more cooperative objects 122 a-122 n. Both the positioningantennas 152 and the tracking antennas 154 may receive the N uniquelycoded signals 113 transmitted from the SDA 110, the reflected versions114 of the N uniquely coded signals and the modified versions 117 of theN uniquely coded signals 113 transmitted from the one or morecooperative objects 122 a-122 n. It should be understood that for somearrangements of the platform positioning antennas 152 and platformtracking antennas 154 and respective signal processing circuits theremay be situations where a frequency shift used by a transponder in acooperative object 122 is large enough that the processing circuitscoupled to the tracking antennas 154 may tune to a frequency band thatis outside of the detectible range of the positioning antennas and therespective processing circuits. In these arrangements, the trackingantennas 154 and respective processing circuits will receive and processthe modified versions 117 of the N uniquely coded signals 113, while thepositioning antennas 152 and respective processing circuits will receiveand process the N uniquely coded signals 113 sent from the SDA 110.

FIG. 2A illustrates an example embodiment of the SDA 110 introduced inFIG. 1. In the illustrated embodiment, the SDA 110′ includes a SDAsubsystem 201, SDA circuitry 220 and N antenna arrays 228. As indicated,the N antenna arrays 228 define the coordinate system 5 introduced inFIG. 1. The SDA subsystem 201 includes a processor 202, input/output(I/O) interface 203, clock generator 204 and memory 205 coupled to oneanother via a bus or local interface 206. The bus or local interface 206can be, for example but not limited to, one or more wired or wirelessconnections, as is known in the art. The bus or local interface 206 mayhave additional elements, which are omitted for simplicity, such ascontrollers, buffers (caches), drivers, repeaters, and receivers (e.g.circuit elements), to enable communications. In addition, the bus orlocal interface 206 may include address, control, power and/or dataconnections to enable appropriate communications among theaforementioned components.

The processor 202 executes software (i.e., programs or sets ofexecutable instructions), particularly the instructions in theinformation signal generator 211, TX module 213, RX module 214, and codestore/signal generator 215 stored in the memory 205. The processor 202in accordance with one or more of the mentioned generators or modulesmay retrieve and buffer data from the local information store 212. Theprocessor 202 can be any custom made or commercially availableprocessor, a central processing unit (CPU), an auxiliary processor amongseveral processors associated with the SDA subsystem 201, asemiconductor based microprocessor (in the form of a microchip or chipset), and application specific integrated circuit (ASIC) or generallyany device for executing instructions.

The clock generator 204 provides one or more periodic signals tocoordinate data transfers along bus or local interface 206. The clockgenerator 204 also provides one or more periodic signals that arecommunicated via the I/O interface 203 over connection 216 to the TXcircuitry 221. In addition, the clock generator 204 also provides one ormore periodic signals that are communicated via the I/O interface 203over connection 217 to the RX circuitry 222. The one or more periodicsignals forwarded to the SDA circuitry 220 enable the SDA 110′ tocoordinate the transmission of the N uniquely coded signals 113 to the Nantenna arrays 228 via the connections 225 and the reception ofinformative signals from the receiver subsystem 130 via the N antennaarrays 228 or the optional connection 139. The I/O interface 203includes controllers, buffers (caches), drivers, repeaters, andreceivers (e.g. circuit elements), to enable communications between theSDA subsystem 201 and the SDA circuitry 220.

The memory 205 can include any one or combination of volatile memoryelements (e.g., random-access memory (RAM), such as dynamicrandom-access memory (DRAM), static random-access memory (SRAM),synchronous dynamic random-access memory (SDRAM), etc.) and non-volatilememory elements (e.g., read-only memory (ROM)). Moreover, the memory 205may incorporate electronic, magnetic, optical, and/or other types ofstorage media. Note that the memory 205 can have a distributedarchitecture, where various components are situated remote from oneanother, but can be accessed by the processor 202.

The information signal generator 211 includes executable instructionsand data that when buffered and executed by the processor 202 generateand forward a signal or signals that communicate at least P electricalmeasurements made by the first receiver in response to the reflections114 of the N uniquely coded signals 113 transmitted by the N transmitarrays 228, where P is a positive integer. Alternatively, theinformation signal generator 211 includes executable instructions anddata that when buffered and executed by the processor 202 generate andforward a signal or signals that communicate a position and motion (ifany) of the non-cooperative object 120 in the coordinate system 5.

The code store/signal generator 215 includes executable instructions anddata that when buffered and executed by the processor 202 generate andforward a set of N signals that are encoded or arranged in a manner thatenable a receiver of the N signals, such as, the receiver subsystem 130,the platform 150, or both to separately identify each of the N signalsat location separate from the SDA 110′. The TX module 213 includesexecutable instructions and data that when buffered and executed by theprocessor 202 enable the SDA subsystem 201 to communicate a set ofuniquely identifiable signals to a spatially distributed architecture(SDA) of N antenna arrays 228, where N is a positive integer greaterthan or equal to two, the arrangement of the N antenna arrays definingthe coordinate system 5. The TX module 213 includes executableinstructions and data that when buffered and executed by the processor202 enable the SDA subsystem 201 to receive reflected versions 114 ofthe set of uniquely identifiable signals 113 transmitted from the SDA ofN antenna arrays 212 and reflected by the non-cooperative object 120 anddetermine a location of the non-cooperative object 120 in the firstcoordinate system 5 based on a respective time and phase of reflectedversions of the uniquely identified signals and an angular position anda range of the receiver subsystem 130 relative to an origin of the firstcoordinate system 5.

In the context of this document, a “computer-readable medium” can be anymeans that can contain, store, communicate, propagate, or transport theprogram for use by or in connection with the instruction executionsystem, apparatus, or device. The computer-readable medium can be, forexample but not limited to, an electronic, magnetic, optical,electromagnetic, infrared, or semiconductor system, apparatus, device,or propagation medium. More specific examples (a non-exhaustive list) ofthe computer-readable medium would include the following: an electricalconnection (electronic) having one or more wires, a portable computerdiskette (magnetic), a random access memory (RAM), a read-only memory(ROM), an erasable programmable read-only memory (EPROM or Flash memory)(magnetic), an optical fiber (optical), and a portable compact discread-only memory (CDROM) (optical). Note that the computer-readablemedium could even be paper or another suitable medium upon which theprogram is printed, as the program can be electronically captured, viafor instance, optical scanning of the paper or other medium, thencompiled, interpreted or otherwise processed in a suitable manner ifnecessary, and then stored in a computer memory.

FIG. 2B illustrates an alternative embodiment of the SDA circuitry 220′introduced in FIG. 2A. In the illustrated embodiment, the receiversubsystem 130 is in close proximity to the transmit circuitry 221′. Thereceiver subsystem 130 includes antenna 132 and receive circuitry 222.The antenna 132 converts electromagnetic energy in the R reflections ofthe N unique coded signals 114 that arrive at the antenna 132 toelectrical signals. The electrical signals are forwarded to the receivecircuitry 222 where they are filtered and amplified. The transmitcircuitry 221′ includes a master oscillator (MO) 223, a synchronizationclock (SYNC CLK) 224, a set of transmit signal generators 226 a-226 nand a respective set of antennas 228 a-228 n. The master oscillator 223generates a common carrier frequency that is distributed to each of thetransmit signal generators 226 a-226 n and to the synchronization clock224. The synchronization clock 224 adjusts the common carrier frequencyand forwards respective codes to each of the respective transmit signalgenerators 226 a-226 n. The synchronization clock 224 may divide thecommon carrier frequency by a factor before forwarding the codes. Inturn, the transmit signal generators 226 a-226 n modulate the commoncarrier frequency with the respective codes and convert the commoncarrier frequency to a radio frequency. An output of each of thetransmit signal generators 226 a-226 n is coupled to an input of arespective antenna 228 a-228 n. The antennas 228 receive the electricalsignals produced by the transmit signal generators 226 a-226 n andconvert the coded electrical signals to an over-the-air electromagneticwave.

Although the illustrated embodiment shows the transmit signal generators226 a-226 n and antennas 228 a-228 n in a one-to-one relationship, twoor more of the transmit signal generators 226 a-226 n may share anantenna. Preferably, the transmit signal generators 226 a-226 n areaugmented by a digital signal processor (not shown) that spatiallydirects the set of N uniquely coded transmit signals 113 in theenvironment 100. Such directivity or beamforming techniques controllablydirect the radio-frequency electromagnetic energy in a predictable way.Accordingly, a control system (not shown) or other source of informationidentifying a region of interest in the environment 100 may direct theSDA circuitry 220′ to send the set of N uniquely coded transmit signals113 in the general direction of a target or non-cooperative object 120.Similarly, the control system or other source of information identifyinga region in the environment 100 where a platform 150 is expected to belocated may direct the SDA circuitry 220′ to send the set of N uniquelycoded transmit signals 113 in the general direction of the platform 150.

The set of N uniquely coded signals 113 produced by the transmit signalgenerators 226 a-226 n are preferably orthogonal, or nearly orthogonal,to each other. This orthogonal coding enables the individual signals tobe distinguished from one another at the receiver subsystem 130. Thereare common signal coding and signal processing techniques that aresuitable for this purpose, including, for example, time-divisionmultiplexing, frequency-division multiplexing, code-divisionmultiplexing, and polarization coding. For some environments acombination of one or more of these coding and signal processingtechniques can be used to generate a set of signals that do notinterfere with one another and are thus separately identifiable.

The antennas 228 a-228 n are spatially distributed in such a way that asmall positional difference of the non-cooperative object or target 120being tracked produces a relatively large differential path lengthbetween the R reflections of the N uniquely coded signals 114 thatencounter the antenna 132. The antennas 228 a-228 n may be arranged informations that are planar or nonplanar. When supported by a structureor a vehicle the size of the formation will be limited only by thedimensions of the underlying structure or vehicle chosen to support theantennas 228 a-228 n. However supported, the antennas 228 a-228 n arespatially distributed in such a way that a small positional differencebetween an array of antennas 152 arranged on an platform 150 produces arelatively large differential path length between the N uniquely codedsignals 113 that encounter the antennas 152.

FIG. 3A illustrates an example embodiment of the receiver subsystem 130introduced in FIG. 1. In the illustrated embodiment, the receiversubsystem 330 includes a processor 331, I/O interface 333, clockgenerator 334 and memory 335 coupled to one another via a bus or localinterface 332. The bus or local interface 332 can be, for example butnot limited to, one or more wired or wireless connections, as is knownin the art. The bus or local interface 332 may have additional elements,which are omitted for simplicity, such as controllers, buffers (caches),drivers, repeaters, and receivers (e.g. circuit elements), to enablecommunications. In addition, the bus or local interface 332 may includeaddress, control, power and/or data connections to enable appropriatecommunications among the aforementioned components.

The processor 331 executes software (i.e., programs or sets ofexecutable instructions), particularly the instructions in the locationmodule 336, motion module 337 and information signal logic 338 stored inthe memory 335. The processor 331 in accordance with one or more of thementioned modules or logic may retrieve and buffer data from the localinformation store 339. The processor 331 can be any custom made orcommercially available processor, a CPU, an auxiliary processor amongseveral processors associated receiver subsystem 330, asemiconductor-based microprocessor (in the form of a microchip or chipset), an ASIC or generally any device for executing instructions.

The clock generator 334 provides one or more periodic signals tocoordinate data transfers along bus or local interface 332. The clockgenerator 334 also provides one or more periodic signals that arecommunicated via the I/O interface 333 over connection 342 tocommunicate wirelessly via antenna(s) 132 or connection 139 when thereceiver subsystem 330 is proximal to the SDA 110′. In addition, theclock generator 334 also provides one or more periodic signals thatenable the receiver subsystem 330 to coordinate the transmission ofinformative signals. The I/O interface 333 includes controllers, buffers(caches), drivers, repeaters, and receivers (e.g. circuit elements), toenable communications between the receiver subsystem 330 and the SDAsubsystem 201.

The memory 335 can include any one or combination of volatile memoryelements (e.g., RAM, DRAM, SRAM, SDRAM, etc.) and non-volatile memoryelements (e.g., ROM). Moreover, the memory 335 may incorporateelectronic, magnetic, optical, and/or other types of storage media. Notethat the memory 335 can have a distributed architecture, where variouscomponents are situated remote from one another, but can be accessed bythe processor 331.

The location module 336 includes executable instructions and data thatwhen buffered and executed by the processor 331 generate and forwardinformation to information signal logic 338 such as at least Pelectrical measurements made by the first receiver subsystem 330 inresponse to the reflections 114 of the N uniquely coded signals 113transmitted by the N transmit arrays 228, where P is a positive integer.Alternatively, the location module 336 may be arranged to forward alocation in X, Y, Z coordinates relative to the origin 10 of thecoordinate system 5.

Motion module 337 includes executable instructions and data that whenbuffered and executed by the processor 331 determine and forward motioninformation to information signal logic 338 such motion information mayinclude velocity vector values in X, Y, Z coordinates relative to theorigin 10 of the coordinate system 5.

Information signal logic 338 includes executable instructions and datathat when buffered and executed by the processor 331 generate andforward a signal or signals that communicate a position and motion (ifany) of the non-cooperative object 120 in the coordinate system 5. Insome embodiments, the information signal logic 338 may generate signalsthat provide local information to one or more cooperative objects 122a-122 n. The information signal logic 338 may also generate signals thatinclude one or more configuration parameters intended to be communicatedto respective cooperative objects 122 a-122 n.

As indicated, local information store 339 may include data describing alocal map, chart, floorplan, etc. The local information store 339 mayinclude locations of fixed items in the coordinate system 5 defined bythe SDA 110. The included data may also define one or more preferredpaths, routes, or channels for the platform 150 to use. This includeddata may be communicated directly or indirectly from the receiversubsystem 330 to the platform(s) 150 as may be desired. In addition, thedata in local information store 339 may receive updates or real-timeinformation regarding the environment 100. Such real-time updates mayinclude the position of both fixed structures and moving platforms 150a-150 n in the local environment 100. In some arrangements, the localinformation store 339 may also receive information including theposition and motion (if any) of one or more cooperative objects 122a-122 n present in the environment 100.

FIG. 3B illustrates a functional block diagram of an embodiment of areceiver subsystem 330′. The receiver subsystem 330′ includes receivercircuitry 222 and one or more tracking antennas 132. The receivercircuitry 222 is configured to operate in conjunction with the transmitcircuitry 221, 221′ shown in FIG. 1 and FIG. 2B. In the illustratedarrangement, the receiver circuitry 222 includes a demodulator (DEMOD)350, matched filter bank 360 and a position calculating processor 331′.The demodulator 350 receives respective signals from the synchronizationclock 224 (FIG. 2B) and the master oscillator 223 (FIG. 2B) as well aselectrical signals from the tracking antennas 132 on connection 342. Thetracking antenna(s) 132 receives electromagnetic energy transmitted bythe transmit circuitry 221 (FIG. 2A) and reflected off of thenon-cooperative object or target 120 being tracked. The tracking antenna132 may be a single antenna or an array of antennas. For ease ofdiscussion, it will be assumed that the tracking antenna 132 is a singleantenna. The demodulator 350 receives the carrier frequency from themaster oscillator 223 and the synchronization clock 224 from the SDAcircuitry 220′, which enable the demodulator 350 to demodulate anddecode the R reflections of the N uniquely coded signals 114. A matchedfilter bank 360 of the receiver circuitry 222 receives the demodulatedsignal from the demodulator 350 and filters the signal to separate thereflections of the N uniquely coded signals 114 from one another anddetermine the time, T, and phase, D, of each respective signal. Asfurther indicated in FIG. 3B, separate time, T(r), and phase, ON signalsare forwarded to the position calculating processor 331′, whichdetermines present X, Y, Z coordinate values in the coordinate system 5.In this way, the position calculating processor 331′ determines apresent position of the non-cooperative object 120. In addition, theposition calculating processor 331′ uses separate instances of presentX, Y, Z coordinate values separated by a known time to determine achange in position of the non-cooperative object 120 over the knowntime. The position calculating processor 331′ divides the respectivechanges in position in each of the three coordinate directions todetermine a velocity of the non-cooperating object 120 in each of the X,Y, and Z directions of the coordinate system 5. In addition, theposition calculating processor 331′ can apply similar logic to determinea present position and motion (if any) of a cooperative object 122.

FIG. 4A illustrates a functional block diagram of an embodiment of aplatform 400. In the illustrated embodiment, the platform 400 includes aprocessor 411, I/O interface 413, clock generator 414 and memory 415coupled to one another via a bus or local interface 412. The bus orlocal interface 412 can be, for example but not limited to, one or morewired or wireless connections, as is known in the art. The bus or localinterface 412 may have additional elements, which are omitted forsimplicity, such as controllers, buffers (caches), drivers, repeaters,and receivers (e.g. circuit elements), to enable communications. Inaddition, the bus or local interface 412 may include address, control,power and/or data connections to enable appropriate communications amongthe aforementioned components.

The processor 411 executes software (i.e., programs or sets ofexecutable instructions), particularly the instructions in the locationmodule 431, motion module 432, orientation module 433 and guidancemodule 434 stored in the memory 415. The processor 411 can be any custommade or commercially available processor, a CPU, an auxiliary processoramong several processors associated with the platform 400, asemiconductor-based microprocessor (in the form of a microchip or chipset), an ASIC or generally any device for executing instructions.

The clock generator 414 provides one or more periodic signals tocoordinate data transfers along bus or local interface 412. The clockgenerator 414 also provides one or more periodic signals that arecommunicated via the I/O interface 413 over connection 417 tocommunicate wirelessly via antenna(s) 152 or over connection 416 viaoptional antenna 154. In addition, the clock generator 414 also providesone or more periodic signals that enable the platform 400 to coordinatethe transmission of informative signals. The I/O interface 413 includescontrollers, buffers (caches), drivers, repeaters, and receivers (e.g.circuit elements), to enable communications between the platform 150 andoptional platforms 150 a-150 n.

The memory 415 can include any one or combination of volatile memoryelements (e.g., RAM, DRAM, SRAM, SDRAM, etc.) and non-volatile memoryelements (e.g., ROM). Moreover, the memory 415 may incorporateelectronic, magnetic, optical, and/or other types of storage media. Notethat the memory 415 can have a distributed architecture, where variouscomponents are situated remote from one another, but can be accessed bythe processor 411.

The location module 431 includes executable instructions and data thatwhen buffered and executed by the processor 411 generate and forwardinformation to information signal generator 435 such as an platformlocation in X, Y, Z coordinates relative to the origin 10 of thecoordinate system 5. The motion module 432 includes executableinstructions and data that when buffered and executed by the processor411 determine and forward motion information to information signalgenerator 435. Such motion information may include velocity vectorvalues in X, Y, Z coordinates responsive to motion of the platform 400relative to the origin 10 of the coordinate system 5. The orientationmodule 433 includes executable instructions and data that when bufferedand executed by the processor 411 determine and forward orientationinformation to information signal generator 435. Such orientationinformation may include a roll angle and an orientation vector in X, Y,Z coordinates responsive to a present condition of the platform 400relative to the origin 10 of the coordinate system 5. When suchorientation information is recorded and observed over time a roll rateover a select period of time may be determined.

Generally, a roll axis or longitudinal axis passes through a missile,projectile or aircraft from a respective nose to a respective tail. Anangular displacement about this axis is called bank. A pilot of a wingedaircraft changes the bank angle by increasing lift on one wing anddecreasing it on the other. The ailerons are the primary controlsurfaces that effect bank. For fixed wing aircraft, the aircraft'srudder also has a secondary effect on bank. A missile will use othercontrol surfaces to achieve a desired bank angle, while a projectile maybe launched with an intentional roll rate that rotates or spins theprojectile about its longitudinal axis.

The term pitch is used to describe motion of a ship, aircraft, orvehicle about a horizontal axis perpendicular to the direction ofmotion. A pitch axis passes through the aircraft from wingtip towingtip. Pitch moves the aircraft's nose up or down relative to thepitch axis. An aircraft's elevator is the primary control surface thateffects pitch. Yaw is a term used to describe a twisting or oscillationof a moving ship or aircraft around a vertical axis. A vertical yaw axisis defined to be perpendicular to the wings and to the normal line orpath of flight with its origin at the center of gravity and directedtowards the bottom of the aircraft. Relative movement about the yaw axismoves the nose of the aircraft from side to side. An aircraft's rudderis a control surface that primarily effects yaw.

A roll rate and an orientation of the platform 150 can be determinedfrom a comparison of the polarization of signals transmitted from theantennas 228 a-228 n with respect to a gravity (or up-down vector) thatmay align with the Z direction of the coordinate system 5. By aligningthe polarization of the transmitted signals with the polarization of theantennas 152 a-152 n the orientation of the up-down vector can betracked in time to provide the pitch, roll, and yaw orientation of theplatform 150 as a function of time in the coordinate frame 5. Inaddition, a similar alignment of the polarization of the transmittedsignals with the polarization of the optional antenna(s) 154 theorientation of the up-down vector can be tracked in time to provideadditional information concerning the pitch, roll and yaw orientation ofthe platform 150 as a function of time. For missiles and projectiles,the antennas 152 a-152 n may be rearward facing whereas optionalantenna(s) 154 may be forward facing. For these form factors,orientation information in the form of pitch and yaw information may bedetermined from signals received at both the antennas 152 a-152 n andthe antenna(s) 154, while roll orientation information may be determinedsolely from the antennas 152 a-152 n.

Alternatively for these form factors, platform orientation includingeach of pitch, yaw and roll may be determined from the signals receivedby the antennas 152 a-152 n alone, from the signals received by theantenna(s) 154 alone, or platform orientation including pitch, yaw androll maybe determined from signals received by the antennas 152 a-152 nand the antenna(s) 154.

This orientation information is sent to the guidance/navigation module434 which includes executable instructions and data that when bufferedand executed by the processor 411 generate and forward information orcontrol signals to one or more control systems (not shown) of theplatform 400. Such control systems may be arranged to navigate orotherwise direct operation of the platform 400 in accordance withinformation from various sensors in combination with information inlocal information store 438. As described, the position and motion (ifany) of the non-cooperative object 120 in the coordinate system 5 arecommunicated to the platform 400. In environments that includecooperative objects 122 a-122 n with suitably arranged transponders, theplatform 400 may also receive the position and motion (if any) of thecooperative objects 122 a-122 n. As described, cooperative objects 122a-122 n may be uniquely identified using a transponder that is arrangedor directed to apply a separately identifiable modification to theuniquely coded signals 113. For example, a time modification couldchange the time of retransmit to identify the cooperative object. Toidentify a select cooperative object 122, the modified signal can betransmitted using a time code (staggered pulses that represent a uniquetime sequence). By way of further example, the phase structure can alsobe modified by multiplying a sequence of SDA waveforms by a sequence ofphase rotations that uniquely identify the object. The position andmotion of the cooperative objects 122 a-122 n may be communicated to theplatform 400 via the receiver subsystem 130 and the SDA 110. Inaddition, the position, motion and orientation of the platform 400 areself-determined in the coordinate system 5. The position and motion (ifany) of the platform 400 in conjunction with data in the localinformation store 438 (including location and motion (if any) of thenon-cooperative object 120 and cooperative objects 122 a-122 n) areforwarded to the guidance/navigation module 434. Thus, a coordinateconversion is not necessarily required on the platform 150. One or morecontrol signals generated by the guidance/navigation module 434controllably direct the platform 400 with respect to the non-cooperativeobject 120 and the one or more cooperative objects 122 (when present) inlight of the local information describing conditions in the environment100.

However, in some embodiments the platform 400 may be arranged to receiveinformation concerning the non-cooperative object 120 from an alternatesignal source that will typically be in a coordinate frame that isdifferent from that defined by the coordinate system 5. For example, thealternate signal source 180 may provide a location and motion (if any)of the non-cooperative object 120 in a GPS format. When this is thecase, an optional conversion module 436 may be arranged with executableinstructions and data that when buffered and executed by the processor411 perform a coordinate conversion to translate a GPS data format tothe coordinate system 5. Alternatively, the conversion module 436 may becapable of translating information identifying the location, motion andorientation of the platform 400 in the coordinate system 5 to the GPSdata format received from the alternate signal source 180. Uponconversion, the converted information may be communicated to theguidance module 434 and or forwarded to one or more control systemsprovided on the platform 150.

As further explained in association with an optional embodimentillustrated in FIG. 1, the platform 150 may be a member of a group ofsimilarly configured platforms 150 a-150 n. When this is the case, theplatform 400 may be arranged with an optional coordination module 437that includes executable instructions and data that when buffered andexecuted by the processor 411 receives information from at least twoother members of the remaining platforms 150 a-150 n. The sharedinformation includes the respective self-determined position, motion andorientation in the coordinate frame 5 and the determined position andmotion (if any) of the non-cooperative object 120 in the coordinateframe 5. The coordination module 437 may further enable the platform 400to communicate a self-determined position, motion and orientation andthe calculated position of the non-cooperative object 120 in thecoordinate frame 5 to other members of the group of platforms.Furthermore, the platform 400 may be arranged to generate a guidancesolution for one or more of the other members of the group of platforms150 a-150 n.

FIG. 4B illustrates a functional block diagram of an embodiment of aplatform 400′. The platform 400′ includes platform circuitry 450, one ormore positioning antennas 152 a-152 n and one or more optional antennas154. The platform circuitry 450 is configured to operate in conjunctionwith signals from the transmit circuitry 221, 221′ shown in FIG. 1 andFIG. 2B. In the illustrated arrangement, the platform circuitry 450includes a summing node 405, receiver demodulator (RX/DEMOD) 410,matched filter bank 420 and a position calculating processor 411′. Theplatform circuitry 450 further includes a phase-locked loop (PLL) 402,local oscillator (LO) 404, and a local clock 406. The LO 404 provides aclock signal to the receiver demodulator 410 that is at the samefrequency as the MO 223 of the SDA circuitry 220, which enables thereceiver demodulator 410 to locate the set of uniquely coded signals 113transmitted from the SDA 110. The local clock 406 is used by thereceiver demodulator 410 to demodulate the set of uniquely coded signals113. The LO 404 and the local clock 406 preferably are synchronized tothe MO 223 and the synchronization clock 224, respectively, just beforeor shortly after launch of a missile, or deployment of the platform 150by using the PLL 402 in the platform circuitry 450 to phase align theclock signal generated by LO 404 with the clock signal generated by MO223. The positioning antenna(s) 152 a-152 n receive electromagneticenergy directly transmitted by the transmit circuitry 221 (FIG. 2A). Thepositioning antenna 152 may be a single antenna or an array of antennas.However arranged, the summing node 405 receives the separate electricalsignals provided by the positioning antenna 152 and forwards a compositesignal to the receiver demodulator 410. The receiver demodulator 410receives the carrier frequency from the local oscillator 404 and thesynchronization clock signal from the local clock 406, which enable thereceiver demodulator 410 to demodulate and decode the N uniquely codedsignals 113. A matched filter bank 420 receives the demodulated signalsfrom the receiver demodulator 410 and filters the signals to separatethe N uniquely coded signals 113 from one another and determines thetime, T, and phase, ϕ, of each respective signal. As further indicatedin FIG. 4B, separate time, T(r), and phase, ϕ(r) signals are forwardedto the position calculating processor 411′, which determines present X,Y, Z coordinate values in the coordinate system 5. In this way, theposition calculating processor 411′ determines a present position of theplatform 150. In addition, the position calculating processor 411′ usesseparate instances of present X, Y, Z coordinate values separated by aknown time to determine a change in position of the platform 150 overthe known time. The position calculating processor 411′ divides therespective changes in position in each of the three coordinatedirections to determine a velocity of the platform 150 in each of the X,Y, and Z directions of the coordinate system 5.

As indicated in the illustrated embodiment, the platform 400′ may bearranged with a receiver 460 for receiving over-the-air informationsignals. The over-the-air information signals may include informationsignal 115 generated and transmitted from the SDA 110 or informationsignal 185 generated and transmitted from an alternate signal source180, which may include information including a position of anon-cooperative object 120. The electromagnetic waves in theover-the-air information signals are converted to electrical signals bythe antenna 465. The electrical signals may be filtered, demodulated andamplified to convey location and motion information responsive to thenon-cooperative object 120. Furthermore, the electrical signalsconverted by the antenna 465 may be buffered over time at the receiver460 to determine changes in each of the X, Y, and Z coordinates over aspecified time. When the over-the-air signals are generated andtransmitted from the SDA 110, the location and velocity of thenon-cooperative object 120 are identified using X, Y, Z coordinates inthe coordinate system 5. When the over-the-air signals are transmittedfrom an alternative signal source 180, the location and velocity of thenon-cooperative object 120 may be provided in an alternate coordinatesystem different from the coordinate system 5. For example, the locationof the non-cooperative object 120 may be provided in GPS coordinates orother three-dimensional coordinate systems. When the location of thenon-cooperative object 120 is provided in a coordinate system that isdifferent from the coordinate system 5, the platform processor 151 orsome other processor will perform a coordinate transformation.Preferably, the platform processor 151 will convert or transform thelocation of the non-cooperative object 120 to the coordinate system 5.

As further indicated in the illustrated embodiment, the platform 400′may optionally be arranged with one or more tracking antennas 154. Whenso provided, the one or more tracking antennas 154 receive M reflectedversions 114 of the N uniquely coded signals 113, where M is an integerless than or equal to N. For ease of discussion, the tracking antenna154 is a single antenna. The electrical signal(s) received by thetracking antenna(s) 154 are forwarded to the receiver demodulator 410.The receiver demodulator 410 demodulates the reflected versions of the Nuniquely coded signals. The demodulated signals are forwarded to thematched filter bank 420, which separates the reflected versions 114 ofthe N uniquely coded signals 113 from each other. The electrical signalsrepresentative of the over-the-air signals transmitted directly from theSDA 110 to the platform 150 traverse a first set of paths. Whereas, theelectrical signals representative of the reflected versions of theover-the-air signals as received at the tracking antennas 154 havetraversed from the SDA 110 to the non-cooperative object 120 and fromthere to the platform 150. Consequently, the time and phase of each ofthese reflected signals will not be the same as the time and phase ofthe signals received at the positioning antennas 152. When provided bothsets of signals, the position calculating processor 411′ determines aplatform position and a non-cooperative object position in thecoordinate system 5. In addition, when provided both sets of signalsover time, the position calculating processor 411′ uses separateinstances of present X, Y, Z coordinate values separated by a known timeto determine a change in position of the platform 150 over the knowntime and to determine a change in position of the non-cooperative object120 over the known time. The position calculating processor 411′ dividesthe respective changes in position of each of the platform 150 and thenon-cooperative object 120 in each of the three coordinate directions todetermine a respective velocity of the platform 150 and thenon-cooperative object 120 in each of the X, Y, and Z directions of thecoordinate system 5. In addition, the position calculating processor411′ can apply similar logic to determine a present position and motion(if any) of a cooperative object 122.

For example, let s₁(t-t₀) and s₂(t-t₀) denote two signals transmittedfrom transmitters A and B respectively where t₀ is the time of transmit.Assume that signal s₁ is received at the first receiver at absolute timet₁ and the signal s₂ is received at the second receiver at absolute timet₂. Assuming, a common frequency, an amplitude propagation model forthese signals is defined by equation 1 and equation 2.

s ₁(t−t ₀)=^(e2πjf(t) ¹ ^(−t) ⁰ ⁾ and s ₂(t−t ₀)=^(e2πjf(t) ² ^(−t) ⁰⁾   Equations 1 and 2

The phase of the signals is defined by equations 3 and 4.

φ₁=2πf(t ₁ −t ₀) and φ₂=2πf(t ₂ −t ₀)  Equations 3 and 4

The differential time, t_(d), is related to the differential phase,φ_(d), as shown in equation 5.

$\begin{matrix}{t_{d} = {{t_{1} - t_{2}} = {{\frac{1}{2\pi \; f}( {\phi_{1} - \phi_{2}} )} = \frac{\phi_{d}}{2\pi \; f}}}} & {{Equation}\mspace{14mu} 5}\end{matrix}$

Thus, the time difference and phase difference are linearly related.Therefore, the terms time difference and phase difference refer toequivalent measured quantities up to a multiplier and resolving anyambiguities in phase.

A position calculating processor 131 of the receiver subsystem 130performs a position-calculating algorithm, which calculates the X, Y andZ Cartesian (or polar) coordinates of the non-cooperative object 120 andthe velocity of the non-cooperative object in the X, Y and Z Cartesian(or polar) directions in coordinate system 5 determined by the locationof the antenna arrays 112 in the SDA architecture 110. The manner inwhich these calculations are made is described below with reference toFIGS. 5-9. The position and velocity information output by the processor131 is then sent to the SDA 110 via connection 139 or wirelesscommunication link 140. In turn, the SDA 110 transmits or communicatesthe position and motion of the non-cooperative object 120 to theplatform 150 where a guidance solution is computed using the interceptorposition and motion computed on the platform.

The use of multiple fixed polarized positioning antennas 152 a-152 n ora single rotating polarized positioning antenna 152 at the platform 150enable the roll rate and orientation of the platform 150 with respect toa gravity vector to be determined. The polarization of the signalstransmitted by the antennas 228 a-228 n can be arranged to align with aknown up-down vector (gravity) at the location of the SDA 110. Byaligning the polarization of the transmitted signals with thepolarization of the antennas 152 a-152 n the orientation of the up-downvector can be tracked in time to provide the pitch, roll, and yaworientation of the platform 150 as a function of time in the coordinateframe 5 determined by the location of the antennas 228 a-228 n of theSDA 110. This orientation information is sent to the guidance system(not shown) of the platform 150.

Once the processor 151 of the platform 150 receives the coordinates ofthe position and velocity of the platform 150 and the coordinates of theposition and velocity of the non-cooperative object 120, a guidancesolution is computed and the guidance system of the platform 150 makesany necessary correction to the flight path of the platform 150 toensure that it is on course to intercept the non-cooperative object 120.It should be noted that because the position and velocity of theplatform 150 and of the non-cooperative object 120 are in the samecoordinate frame, no frame alignment is needed, which provides theaforementioned advantages over the conventional command guidance firecontrol systems.

The processor 151 of the platform 150 could be responsible for computingthe guidance solution or, alternatively, a separate processor on theplatform 150 (not shown) could perform the task of computing theguidance solution. The platform 150 may be further arranged with anavigation control system or autopilot system (not shown) that includesa processor that converts the guidance solution into actual guidancecommands or control signals that are then delivered to one or moreservos or other control signal converters that adjust the position ofone or more control surfaces (not shown) arranged on the platform 150.Such control systems change the direction of the platform 150 based onthe guidance commands or control signals. The processor 151 of theplatform 150 may generate the guidance commands and deliver them to theguidance system, or a processor of the autopilot system may perform thisfunction. As will be understood by persons of skill in the art, in viewof the description provided herein, processing tasks may be performed bya single processor or distributed across multiple processors.

The receiver subsystem 130 and the platform 150 determine differentialtime and/or phase and absolute time-of-arrival measurements of theuniquely coded signals transmitted from the set of antennas 228 a-228 n.These time-based measurements and knowledge of the speed of the signalpropagation enable calculations to be made of the differential andabsolute path lengths over which the signals have traveled. Thesemeasured path lengths, in conjunction with knowledge of the distributedlayout of the antennas 228 of the SDA 110 and the known spatialrelationship between the receiver subsystem 130 and the SDA 110, areused by the processor 131 and the processor 151 in the receiversubsystem 130 and the platform 150, respectively. Based on thisinformation, the receiver subsystem 130 determines the position andmotion of the non-cooperative object 120 relative to the SDA 110 and theplatform 150 self-determines its position and motion relative to the SDA110.

The determinations made by the receiver subsystem 130 are communicatedto the SDA 110 and transmitted over-the-air to the platform 150. Thesedeterminations are then combined with the determinations made by theprocessor 151 of the platform 150 to provide the platform 150 with theposition and motion of the non-cooperative object 120 relative to theplatform 150 to compute a guidance solution.

The times-of-arrival of the transmitted uniquely coded signals 113 atthe receiver subsystem 130 and the platform 150 are measured and thedifferences between these times are calculated. The differential timecalculations obtained by the receiver subsystem 130 and knowledge of thelayout of the SDA 110 and its spatial relationship with the antenna(s)132 of the receiver subsystem 130 are used by the processor 131 todetermine the path lengths from the antennas 228 a-228 n to thenon-cooperative object 120. The differential time calculations obtainedby the platform 150 and knowledge of the layout of the SDA 110 are usedby the processor 151 to determine the path lengths from the antennas 228a-228 n to the positioning antenna(s) 152 on the platform 150. Becausethe clocks that are used by the transmit signal generators 226 a-226 n,the receiver subsystem 130 and the platform 150 are synchronized, asdescribed above with reference to FIG. 2B, FIG. 3B and FIG. 4B, theabsolute arrival times of the signals can be determined by the receiversubsystem 130 and the platform 150. The absolute arrival times can beused to determine the absolute ranges, and consequently, the fullposition vectors can be determined. These same principles can be appliedto locate and determine relative motion (if any) of cooperative objectsthat receive, modify and transmit modified versions of the N uniquelycoded signals.

The processor 131 and the processor 151 determine the path lengths bymeasuring the difference in time-of-arrival of the signals as describedabove or by measuring the differential phase φ of the signals. Use ofrelative phase measurements is called interferometry. Interferometryrequires coherence in the transmit signal generators 226 a-226 n. Whileeither technique can be used to calculate the angle-of-arrival, therelative accuracy of the measurements is not the same. Interferometryimproves the accuracy of this process by comparing the relative phaseshifts of the received signals to provide a very accurate anglemeasurement.

In example embodiments motion is determined using the determined rangeand the differential change in the range of the signal propagationpaths. Once the differential change in each path length has beendetermined, the combination of these values allows the platform 150 toself-determine its motion and allows the receiver subsystem 130 todetermine the motion of the non-cooperative object 120 by multiplyingthe unit position vector by the differential path length change. Thealgorithms that are executed by the processor 151 and the processor 131to compute the positions and motions of the non-cooperative object 120and of the platform 150, respectively, include straight-forwardtrigonometric calculations as will now be described with reference toFIGS. 5-9.

FIG. 5 is a schematic diagram that illustrates the manner in which theposition and orientation of a target or non-cooperative object 120relative to the receiver platform 130 of FIG. 1 can be determined in twodimensions using trigonometry. An example spatial relationship (not toscale) between a set of antennas, ANT₁ and ANT₂, a receiver, RX1, and areflective non-cooperative object or target 120 are shown in twodimensions in FIG. 5. An origin 10 is located equidistant between ANT₁and ANT₂ when the distance a1 between the origin 10 and ANT₁ is equal tothe distance a₂ between the origin 10 and the ANT₂. Stated another way,the origin 10 is the overall phase center of a spatially-distributedarchitecture of N antenna arrays comprising ANT₁ and ANT₂. The range,|RSDC_(toTARGET)| from center of the SDA (i.e., origin 10) to the target120 and angular position, θ_(TARGET), of the object relative to theorigin 10 can be determined by the receiver subsystem 130 based on theknown spatial relationship between the origin 10 and the antenna 132 byusing the measurements of the difference in time-of-arrival of thesignals as described above or the differences in the phase φ of thesignals. The range, |RSDC_(toRX1)|, from origin 10 to the antenna 132and the angular position, θ_(RX), of the antenna 132 relative to theorigin 10 are known a priori. Consequently, the range, |RRX_(toTARGET)|, from the antenna 132 to the target 120 and the angle,(φ_(object), of the target relative to the antenna 132 can be determinedby the processor 131 of the receiver subsystem 130 using trigonometry,as will be understood by persons skilled in the art in view of thedescription provided herein.

FIG. 6 is a schematic diagram that illustrates the manner in which theposition and orientation (not to scale) of the second receiver locatedon an platform 150 remote from the origin 10 defined by the SDA 110 ofFIG. 1 can be determined in two dimensions using trigonometry. In FIG.6, a₁, a₂, RANT_(1toRx2), RANT_(2toRx2), and RSDC_(toRX2) are vectors.Given a known distance (| a₁|,|−a₂|) between the respective antennasANT₁ and ANT₂ and the origin 10, the differential distance(|RANT_(1toRx2)|−|RANT_(2toRx2)|) from ANT₁ and ANT₂ to RX2 can becomputed. RX2 is the overall phase center of the positioning antenna(s)152 located on the platform 150. Using this information, the angleθ_(RX) can be determined, where θ_(RX) is the angle between theperpendicular to the line between the antennas ANT₁ and ANT₂ and theline to the antennas 152 from the origin 10. This may be accomplished bymeasuring the difference in time-of-arrival of the signals from eachantenna 228 a-228 n (FIG. 2B) and multiplying by the speed of the signalpropagation or by relating the phase difference to time difference. Intwo dimensions, the differential range measurements and the angle θ_(RX)are related by the equation,

|RANT_(1toRX2)|−|RANT_(2toRx2)|=(|a ₁ −a ₂|)sin θ_(RX),  Equation 6

If the receiver clock (e.g., clock 406) is synchronized with thetransmitter clock (e.g., synchronization clock 224), it is possible todetermine not only the relative difference in arrival time of thesignals transmitted from ANT₁ and ANT₂ to RX2, but also the absolutearrival time of the transmitted signals at RX2. Using this information,it is then possible to determine the distance from RX2 to each of theantennas ANT₁ and ANT₂. Using standard trigonometric equations, thedistance from RX2 to the origin 10 can be determined. As will now bedescribed, this two-dimensional system can be extended easily to threedimensions by adding one or more additional antennas and one or morerespective unique codes.

FIG. 7 is a schematic diagram that illustrates the manner in which theposition and orientation (not to scale) of the second receiver locatedon an platform 150 remote from the origin 10 defined by the SDA 110 ofFIG. 1 can be determined in three dimensions. The example embodimentshows relationships between three antennas, ANT₁, ANT₂ and ANT₃, and thepositioning antennas 152 in the platform 150, labeled RX2, in threedimensions. As indicated, there are two angles (θ_(RX), Ψ_(RX)) thatneed to be computed to determine position. However, these angles can bedetermined from algebraic equations with well-established solutions. Thesolution to the resulting position equations follows, under theassumption of synchronized clocks and that the coordinate frame center(e.g., origin 10) is located at the centroid of the antenna locationvectors a₁, a₂, a₃, i.e.,

$\begin{matrix}{{{Tx}\mspace{14mu} {Center}} = {\begin{pmatrix}0 & 0 & 0\end{pmatrix} = \frac{a_{1} + a_{2} + a_{3}}{3}}} & {{Equation}\mspace{14mu} 7}\end{matrix}$

And it follows that

${{{RSDC}_{{toRX}\; 2}}^{2} = {\frac{{{RANT}_{1{toRX}\; 2}}^{2} + {{RANT}_{2{toRX}\; 2}}^{2} + {{RANT}_{3{toRX}\; 2}}^{2}}{3} - \frac{{a_{1}}^{2} + {a_{2}}^{2} + {a_{3}}^{2}}{3}}},$

and assuming Tx Center=(0 0 0),

${{RSDC}_{{toRX}\; 2} \cdot a_{1}} = \frac{{{RANT}_{1{toRX}\; 2}}^{2} - {{RSDC}_{{toRX}\; 2}}^{2} - {a_{1}}^{2}}{2}$${{RSDC}_{{toRX}\; 2} \cdot a_{2}} = \frac{{{RANT}_{2{toRX}\; 2}}^{2} - {{RSDC}_{{toRX}\; 2}}^{2} - {a_{2}}^{2}}{2}$${{RSDC}_{{toRX}\; 2} \cdot a_{3}} = \frac{{{RANT}_{3{toRX}\; 2}}^{2} - {{RSDC}_{{toRX}\; 2}}^{2} - {a_{3}}^{2}}{2}$

The term RSDC_(to)RX2 represents the vector from the center of the arrayof N antennas or origin 10, to the receiver center, RX2, or antenna 152(when one antenna is used). The terms RANT_(1toRx2), RANT_(2toRx2),RANT_(3toRX2) represent the vectors from the antennas ANT₁, ANT₂ andANT₃, respectively, to RX2. The terms a₁, a₂, and a₃ represent thevectors from the origin 10 to each of the antennas ANT₁, ANT₂ and ANTT₃,respectively. The derivation of these equations will be understood bythose skilled in the art in view of this description.

FIG. 8 is a diagram that illustrates the relationship, in twodimensions, between two antennas, ANT₁ and ANT₂, one receiver platformantenna 132, RX1, and a target or non-cooperative object 120 beingtracked. It should be noted once again, that in three dimensions, thereare more choices for how to arrange the antennas. In addition, there aremore equations to be solved and two angles that need to be computed todetermine position. However, as indicated above, the equations that maybe used for this are algebraic equations with well-established solutionsthat will be understood by those skilled in the art.

Because the position of the first receiver subsystem 130 relative theSDA 110 is known a priori, the position of any object reflecting theuniquely coded transmitted signals 113 towards the first receiversubsystem 130 and more specifically the antenna (or RX1) 132 can bedetermined. With reference to FIG. 8, the values of the vectors (a₁, a₂,RTC_(toRx1)) and the angles θ_(RX) and Ø_(RX1) are all known, while thevalues of the vectors (R_(TCtoTARGET), RRX1_(toTARGET),RANT_(1toTARGET), RANT_(2toTARGET)) and the angles θ_(TARGET) andØ_(TARGET) are unknown. However, because the signals that reflect off ofthe object share a common path along RRX1_(toTARGET), the difference inarrival times at the receiver subsystem 130 is entirely due to thedifference in length of the vectors RANT_(1toTARGET) andRANT_(2toTARGET). This information is enough to allow the angle of thetarget relative to the antennas 228 a-228 n to be calculated in thecoordinate frame 5 defined by the positions of the antennas. In twodimensions, assuming |a₁|=|a₂|, the differential range measurements andthe angle relative to the SDA center or origin 10 are related by theequation:

|RANT_(1toTARGET)|−|RANT_(2toTARGET)|=(|a ₁ −a ₂|)sin θ_(TARGET).

As stated above, if the local clocks of the SDA 110 and the receiversubsystem 130 are synchronized, it is possible to determine not only therelative difference in arrival time of the signals from each antennas228 a-228 n, and consequently the angular position of the target 120,but also the absolute arrival time of the transmitted signals, which, inconjunction with the known position of the receiver subsystem 130relative to the origin 10, gives the range of the target 120 in thecoordinate system 5 determined by the location of the antennas 228 inthe SDA 110. However, unlike the calculation used to determine the rangeof the receiver, this calculation requires the simultaneous solution ofintersecting ellipses. Methods exist, such as, for example, the gradientdescent and Newton-Raphson methods, that are suitable for use with theinvention to solve the resulting set of equations. Those skilled in theart will understand the manner in which these or other methods may beused to make these calculations. This two-dimensional system can beextended easily to three dimensions by using one or more additionalantennas that broadcast one or more respective uniquely coded signals.

FIG. 9 is a schematic diagram that illustrates spatial relationships inan example arrangement of a SDA 110, a receiver subsystem 130 withmultiple antennas and a non-cooperative object or target 120 of FIG. 1in two dimensions. In this embodiment, two spatially distributedreceivers RX₁ and RX₂ are coupled to or provided by the receiverplatform 130. A center 910 of the spatially-distributed receiverantennas RX₁ and RX₂ is located equidistant between RX₁ and RX₂ when thedistance b₁ between center 910 and RX₁ is equal to the distance b₂between center 910 and the RX₂. Stated another way, the center 910 isthe overall phase center of a spatially-distributed architecture of Nantenna arrays comprising RX₁ and RX₂. The manner in which the positionof the target 120 can be calculated using the path length differencesresulting from the use of both distributed SDA antennas that defineorigin 10 and distributed receivers that define a phase center 910 willnow be described with reference to FIG. 9. In this example, it isassumed that the values of the vectors a₁, a₂, b₁, b₂, RTC_(toRXc) andangles θ_(RX) and Ø_(RX) are all known, while the values of the vectorsRTC_(toTARGET), RANT_(1toTARGET), RANT_(2toTARGET), and RRX_(1toTARGET)and the angles θ_(Target) and Ø_(TARGET) are unknown. However, becausethe signals that reflect off of the object share a common path alongR_(RXANT1toTARGET) and a separate common path along R_(RXANT2toTARGET),the difference in arrival times at the respective receiver platformantennas is entirely due to the difference in the lengths of the vectorsRANT_(1toTARGET) and RANT_(2toTARGET). This information is enough toallow the angle of the object, θ_(TARGET), relative to the origin 10 tobe calculated in the coordinate frame 5 defined by the location of theantennas 228 a-228 n in the SDA of antenna arrays 112. In two dimensionsassuming |a₁|=|a₂|, the differential range measurements and the angle ofthe object relative to the origin 10 are related by the equation:

|RANT_(1toTARGET)|−|RANT_(2toTARGET)|=(|a ₁ −a ₂|)sin θ_(TARGET).

In two dimensions assuming b₁=b₂, the differential range measurementsand the angle of the target relative to the center 910 of the receiverantennas RX₁ and RX₂ are related by the equation:

|RXANT_(1toTARGET)|−|RXANT_(2toTARGET)|=(|b ₁ −b ₂|)sin ϕ_(TARGET).

The length or range of the vector RXANT_(1toTARGET) can be determined bythe difference of the total range of the reflected versions of theuniquely coded signals received at RX₁ and the lengths of the vectorsRANT_(1toTARGET) and RANT_(2toTARGET). Similarly, the length or range ofthe vector RXANT_(2toTARGET) can be determined by the difference of thetotal range of the reflected versions of the uniquely coded signalsreceived at RX₂ and the lengths of the vectors RANT_(1toTARGET) andRANT_(2toTARGET). This two-dimensional system can be extended to threedimensions.

FIG. 10 illustrates an example embodiment of a method 1000 that can beperformed by SDA 110 to determine a position of a non-cooperative object120 relative to the SDA 110 and to communicate the position to aplatform 150 remote from the SDA 110. The method 1000 begins with block1002 where the SDA 110 transmits a set of uniquely identifiable signalsfrom respective spatially-distributed antenna arrays 112. In block 1004,a receiver or receiver subsystem 130 located at a known positionrelative to the antenna arrays 112, receives reflected versions 114 ofthe uniquely identifiable signals 113 reflected from the non-cooperativeobject 120. In block 1006, a processor 131 in communication with thereceiver or receiver subsystem 130 determines a location of thenon-cooperative object 120 relative to a coordinate system 5 defined bythe antenna arrays 112. Thereafter, as indicated in block 1008, the SDA110 communicates the location of the non-cooperative object 120 in thecoordinate system 5 to one or more platforms 150.

FIG. 11 illustrates an example embodiment of a method 1100 that can beperformed by a platform 150. The method 1100 enables the platform 150 toself-determine a platform position in a coordinate system 5 defined by aspatially-distributed architecture of antenna arrays 112 and to useinformation received from the spatially-distributed architecture ofantenna arrays 112 regarding the location of a non-cooperative object120. The platform 150 uses the location of the non-cooperative object120 to guide the platform 150 relative to the non-cooperative object120. The method 1100 begins with block 1102 where a first platformreceiver located on the platform 150 receives a set of uniquelyidentifiable signals from respective spatially-distributed antennaarrays 112. In block 1104, a processor 151 in communication with thefirst platform receiver, determines one or more of position, motion andorientation of the platform in the coordinate system 5 based oncharacteristics of the uniquely identifiable signals 113 transmittedfrom the spatially-distributed architecture of antenna arrays 112. Inblock 1106, the platform 150 receives one or more information signals115 that contain information about the location of the non-cooperativeobject 120 in the coordinate system 5. In block 1108, the processor 151generates a guidance solution based on the position, motion andorientation of the platform 150 relative to the position and motion (ifany) of the non-cooperative object 120 in the coordinate system 5. Inblock 1110, a control signal responsive to the guidance solution isforwarded to a control system on the platform 150 to direct the platform150 relative to the non-cooperative object 120.

The illustrated embodiments provide a system where a platform(s) 150 nolonger has to rely on inertial guidance systems to direct the platform150 on a trajectory or path toward the non-cooperative object or target120. Since the receiver subsystem 130 tracks the location of the target120 and the platform 150 self-locates its position in a commoncoordinate system 5, a processor (e.g., the processor 151) need notperform a coordinate translation before determining a guidance solutionfrom these inputs.

In addition, since tracking of the target 120 by the receiver subsystem130 and the platform 150 self-tracking are performed in a commonreference frame 5 defined by the locations of the antennas 228 a-228 nin the SDA 110, a transition of the responsibility for tracking thetarget or non-cooperative object 120 can be transferred to the platform150 from the receiver subsystem 130 without a need for a coordinatetranslation. The hand off or transfer is efficient as a single filtercan be used for both the N uniquely coded signals 113 and the reflectedversions 114 of the N uniquely coded signals 113, thereby reducing thepossibility of filter transients as a result of the transition. From thetime of transition until interception, the platform 150 continues toself-track while also tracking the target 120. The same principlesdescribed above with reference to FIGS. 5-9 apply to the operationsperformed by the platform 150 to self-track while also tracking thenon-cooperative object or target 120.

In addition, when a platform 150 is arranged with optional antennas 154arranged to receive an indication of the location and motion (if any) ofthe target 120 the platform 150 continues to self-track its position andmotion relative to the origin 10 of the coordinate system 5, while theadditional antenna 154 receives the target tracking information from theexternal source 180 and delivers it to the guidance system (not shown)of the platform 150. For example, the position and motion of the target120 as measured by the external source 180 may be in a coordinate systemdefined by or provided to an inertial sensor (not shown) of the externalsource 180. The platform 150 will receive the information in thatalternative coordinate system from the external source 180 and transformit into the coordinate frame 5 defined by the locations of thetransmitters 228 a-228 n in the SDA 110. The guidance system of theplatform 150 then uses this transformed or converted information toadjust its flight path or direction, if necessary, such that itconverges with the non-cooperative object 120 when so desired.Alternatively, the guidance system (not shown) of the platform 150 usesthe information to adjust its path, if necessary, such that its pathorbits or otherwise avoids the non-cooperative object 120 when sodesired.

FIG. 12 includes a flow diagram illustrating an example embodiment of amethod 1200 for self-determining one or more of a position, motion andorientation in a coordinate system 5 and guiding a platform relative toa remote non-cooperative object 120. The method 1200 begins with block1202 where a first platform receiver 552 located on the platform 500receives a set of uniquely identifiable signals 113 transmitted from aspatially-distributed architecture (SDA) of antenna arrays 112. In block1204, a processor 551 in communication with the first platform receiver552, determines one or more of position, motion and orientation of theplatform 500 in the coordinate system 5 based on characteristics of theuniquely identifiable signals 113 transmitted from the SDA of antennaarrays 112. In block 1206, the platform 500 receives one or moreinformation signals that contain information about the location of anon-cooperative object 120 relative to the platform 500. The informationsignals may be transmitted from another forward-based platform, or maybe in the form of reflected electromagnetic energy from one or moresources. In block 1208, the processor 551 generates a guidance solutionbased on the position, motion and orientation of the platform 500relative to the position and motion (if any) of the non-cooperativeobject 120 in the coordinate system 5. The one or more informationsignals may be combined with the self-determined position, orientationand motion of the platform 500 to also determine the position, motionand orientation of the non-cooperative object 120. In block 1210, acontrol signal responsive to the guidance solution is applied to aguidance system 556 to direct the platform 500 relative to thenon-cooperative object 120.

In block 1212, the platform 500 receives an informational signal 115identifying a present location of the SDA of antenna arrays 112. Inblock 1214, the platform 500 is programmed or configured to confirmand/or adjust a present location of the SDA of antenna arrays 112 and aplatform determined position in the coordinate system 5. As indicated inblock 1216, the platform 500 may optionally be arranged to communicatean informational signal 1420 identifying a location of thenon-cooperative object 120 to proximally located receivers.

As indicated in FIG. 12, the method 1200 is arranged such that thefunctions and operations associated with blocks 1202-1216 may berepeated as may be desired to navigate or otherwise guide the platform500 relative to the non-cooperative object or target 120 in thecoordinate system 5 and to guide and direct one or more optionalinterceptor platforms 600 near the platform 500.

FIG. 13 includes a flow diagram illustrating an example embodiment of amethod 1300 for self-determining one or more of a position, motion andorientation in a coordinate system 5 and guiding a platform relative toa remote non-cooperative object 120. The method 1300 begins with block1302 where a first platform receiver 552 located on the platform 500receives a set of uniquely identifiable signals 113 transmitted from aspatially-distributed architecture (SDA) of antenna arrays 112. In block1304, a processor 551 in communication with the first platform receiver552, determines one or more of position, motion and orientation of theplatform 500 in the coordinate system 5 based on characteristics of theuniquely identifiable signals 113 transmitted from the SDA of antennaarrays 112. In block 1306, the platform 500 receives one or moreinformation signals that contain information about the location of anon-cooperative object 120 relative to the platform 500. The informationsignals may be transmitted from another forward-based platform, or maybe in the form of reflected electromagnetic energy from one or moresources. As illustrated in FIG. 14, the information signal may be in theform of reflected electromagnetic energy 1402 that is received by asensor 1460 or a sensor subsystem supported by the platform 500. Inblock 1308, the processor 551 generates a guidance solution based on theposition, motion and orientation of the platform 500 relative to theposition and motion (if any) of the non-cooperative object 120 in thecoordinate system 5. The one or more information signals may be combinedwith the self-determined position, orientation and motion of theplatform 500 to also determine the position, motion and orientation ofthe non-cooperative object 120. In block 1310, a control signalresponsive to the guidance solution is applied to a guidance system 556to direct the platform 500 relative to the non-cooperative object 120.

In block 1312, the platform 500 generates a platform unique signaldifferent from any of the uniquely identifiable signals transmitted fromthe SDA of antenna arrays 112 and different from other forward-basedplatforms in the system of platforms 1400. In block 1314, the platformis arranged to transmit the platform unique signal such as ininformation signal 1420 toward one or more interceptor platforms 600. Inaddition, as indicated in block 1316, the platform 500 is arranged totransmit a respective information signal identifying a present locationof the platform 500.

As indicated in FIG. 13, the method 1300 is arranged such that thefunctions and operations associated with blocks 1302-1316 may berepeated as may be desired to navigate or otherwise guide the platform500 relative to the non-cooperative object or target 120 in thecoordinate system 5 and to guide and direct one or more optionalinterceptor platforms 600 near the platform 500.

FIG. 14 is a schematic diagram that illustrates an alternativeembodiment of a system of platforms 1400 including a group of variousplatform types navigating in one coordinate system. The improvedtracking and/or guidance system includes a pilot platform 1445 with aspatially-distributed architecture (SDA) 110 or signal generationsub-system 111 that is separated or remotely located from anon-cooperative object or target 120. In the illustrated embodiment, thepilot platform 1445 is collocated or proximally located to a receiversubsystem or first receiver 130. A remote or forward-based platform 500,and one or more second or interceptor platforms 600 a-600 n are separatefrom the pilot platform 1445 with the forward-based platform 500 withinsignal range of the N uniquely coded transmit signals 113 and one ormore informational signals 115 communicated wirelessly from the pilotplatform 1445.

As indicated schematically in FIG. 14, the SDA 110 defines a coordinatesystem 5. The coordinate system 5 includes an origin 10 where an X-axis12, a Y-axis 13, and a Z-axis 14 meet. As further indicatedschematically in FIG. 1, the X-axis 12 is orthogonal or approximatelyorthogonal to both of the Y-axis 13 and the Z-axis 14. In addition, theY-axis 13 is orthogonal or approximately orthogonal to the Z-axis 14.The coordinate system 5 provides a mechanism to spatially define therelative location and orientation of items in the system of platforms1400. While the origin 10 may be defined at any location within or aboutthe SDA 110, the origin 10 is preferably located at the phase center ofthe N antenna arrays 112 forming the SDA 110.

In the illustrated embodiment, the forward-based platform 500 is shiftedor translated in one or more of the X, Y and Z directions with respectto the coordinate system 5.

As described in association with the embodiment illustrated in FIG. 1,the SDA 110 generates and controllably transmits N uniquely codedsignals 113 where N is a positive integer greater than or equal to two.The N uniquely coded signals 113, generated by and transmitted from theSDA 110, impinge or directly encounter the platform 500. In the presentembodiment the SDA 110 may be a fixed station on the ground or a movingstation disposed on a moving platform such as, for example, a ship, anairplane, a flying drone, a truck, a tank, or any other type of suitablevehicle (not shown). In addition to transmitting the uniquely codedsignals from the SDA 110, the pilot platform 1445 generates andtransmits one or more information signal(s) 115 that periodicallyidentify a present location of the pilot platform 1445 in a coordinatesystem. For example, the information signal(s) 115 may include latitude,a longitude and an altitude corresponding to the origin 10 of thecoordinate system 5.

In the example embodiment, the first or forward-based platform 500 isarranged with processing circuitry or a processor 551, memory 555, oneor more antennas 552, transmit and receive subsystems or a transceiversubsystem 553, one or more optional antennas 554, a guidance system 556and a sensor system 1460. The forward-based platform 500 may be fixed toone or more of a missile, a projectile, a ship, an airplane, a flyingdrone, a truck, a tank, or any other type of suitable vehicle or even arelatively small portable device (not shown). When the forward-basedplatform 500 is coupled to or part of a projectile, the platform 500 maybe dropped, launched, expelled or otherwise separated from a ship,airplane, drone, or land-based vehicle. The guidance system 556 isarranged with one or more control systems, an inertial navigation systemand is optionally arranged with a propulsion system. The guidance system556 is capable of controllably directing movement of the forward-basedplatform 500 with respect to the non-cooperative object or target 120,as indicated by a platform vector 1415. The platform vector orV_(PLATFORM) 1415 may have components in one or more of the X-direction12, Y-direction 13 and Z-direction 14 of the coordinate system 5.

The one or more antennas 552 receive the N uniquely coded transmitsignals 113 and the periodic information signal(s) 115 transmitted bythe SDA 110. The received signals are bandwidth filtered, down convertedin frequency and demodulated by the transceiver subsystem 553 beforebeing forwarded to the processor 551. The memory 555 includes one ormore logic modules and data values (not shown) that when controllablyretrieved and executed by the processor 551 enable the processor 551, inresponse to information derived from the N uniquely coded signals 113 asreceived at the antennas 552, to self-determine a position of theplatform 500 in the coordinate system 5. Changes in the location of theplatform 500 relative to the SDA 110 may also be determined by theprocessor 551 or may be determined solely in an inertial navigationsystem (INS) coupled to or otherwise provided in the guidance system556.

Electromagnetic energy 1402 may originate at or within thenon-cooperative object or target 120. Examples of such electromagneticenergy 1402 include RF signals or infrared radiation (IR) emanating fromthe non-cooperative object 120. In addition or alternatively, thenon-cooperative object or target 120 can be identified by reflectedelectromagnetic energy 1404. Examples of such electromagnetic energy1404 includes RF or radar signals, light detection and ranging signalsemanating from a source such as interceptor platform 600 n that aredirected toward and reflected from the non-cooperative object or target120.

The sensor system 1460, which may be an optical system or a radarsystem, receives one or more wireless signals that include informationregarding the relative position or location of the non-cooperativeobject 120 with respect to the forward-based platform 500. An opticalsensor system may include a photosensitive receiver and optical elementsarranged to intercept, collimate and/or focus the received opticalsignal. Alternatively, the optical sensor system may include or controla light source for illuminating the non-cooperative object or target120. When such a light source is integrated with the sensor system 1460,the sensor system will include one or more emitters and correspondingoptical elements to collect, collimate and/or focus emitted light towardthe non-cooperative object or target 120.

In addition, or as part of a preliminary target identification oracquisition process, one or more of the antennas 552 or a dedicatedoptional antenna 554 may receive information identifying the locationand motion (if any) of the pilot platform 1445 as communicated by theSDA 110 via the communication link 115. The forward-based platform 500may further receive information from other communication linkstransmitted from alternative signal sources (not shown) identifying orlocating a search region within which the forward-based platform 500 canobserve the non-cooperating object or target 120. Thus, one or morelogic modules and data values can be communicated to and or stored onthe forward-based platform 500 and transferred to the processor 551 toenable any one of the previously described operational modes.

In one example mode, the first or forward-based platform 500 isprogrammed or otherwise instructed via one or more information signals115 to acquire an optical signal or radar signal reflected by thenon-cooperative object or target 120 and to maintain a pre-definedrelationship over time with respect to the non-cooperative object ortarget 120. For example, the forward-based platform 500 may beprogrammed or otherwise instructed to determine the vector, V_(TAR),defined by the incident reflected optical or radar beam to intercept andcontact the target 120. In another example mode of operation, theforward-based platform 500 may be programmed or otherwise instructed tonavigate about the non-cooperative object or target 120 in a desiredway.

In addition, the one or more antennas 552 and/or the optional antenna554 will periodically or intermittently receive a signal that may beforwarded to one or both of the guidance system 556 and the processor551 from the SDA of antenna arrays 110 to provide updated informationregarding the location of the forward-based platform 500 relative to thecoordinate system 5 defined by the SDA of antenna arrays 110. Inresponse, the INS of the guidance system 556 may be monitored foraccuracy and/or adjusted as may be desired using information provided inthe information signal 115 and information such as a range and angledetermined from the time of arrival and phase differences of the Nuniquely coded transmit signals 113. In addition or alternatively, theguidance system 556 and/or the processor 551 may generate a modifiedcontrol signal using a combination of information from the INS and thesignal from the SDA of antenna arrays 110 to ensure that theforward-based platform 500 is accurately positioned on a course tointercept, orbit or otherwise navigate with respect to thenon-cooperative object or target 120.

In the example embodiment, the second or interceptor platform(s) 600a-600 n is arranged with processing circuitry or a processor, memory,one or more antennas, and a guidance system. The interceptor platform(s)600 a-600 n may be fixed to one or more of a missile, a projectile, aship, an airplane, a flying drone, a truck, a tank, or any other type ofsuitable vehicle or even a relatively small portable device (not shown).When the interceptor platform(s) 600 a-600 n is coupled to or part of aprojectile, the platform 600 a-600 n may be dropped, launched, expelledor otherwise separated from a ship, airplane, drone, or land-basedvehicle. The guidance system is arranged with one or more controlsystems, an inertial navigation system and is optionally arranged with apropulsion system. The one or more antennas may receive the N uniquelycoded transmit signals 113 transmitted by the SDA 110 or may navigatebased on their respective INS as periodically confirmed and/or updatedwith information broadcast from the forward-based platform 500 via theinformation signal 1420. The interceptor platforms 600 a-600 n mayfurther receive vector V_(TAR). In response, the guidance system 656 maygenerate a modified control signal to ensure that the respectiveinterceptor platform 600 a-600 n is on a course to intercept thenon-cooperative object or target 120.

FIG. 15 is a schematic diagram that illustrates another alternativeembodiment of a system of platforms 1500 including a group offorward-based platforms 700 a-700 n and a separate group of(interceptor) platforms 150 a-150 n navigating in multiple coordinatesystems. The improved tracking and/or guidance system includes a firstor primary spatially-distributed architecture (SDA) or signal generationsub-system 110 that is separated or remotely located from anon-cooperative object or target 120. In the illustrated embodiment, theSDA 110 is arranged or located to the same side of each of thenon-cooperative object or target 120, and one or more forward-basedplatforms 700 a-700 n. The system of platforms 1500 is not so limitedand in modified environments the SDA 110 will be spatially located inother relationships with respect to the receiver subsystem 130,platforms 700 a-700 n, and the non-cooperative object or target 120.

As indicated schematically in FIG. 15, the SDA 110 defines a firstcoordinate system 5. The first coordinate system 5 includes an origin 10where an X-axis 12, a Y-axis 13, and a Z-axis 14 meet. As furtherindicated schematically in FIG. 15, the X-axis 12 is orthogonal orapproximately orthogonal to both of the Y-axis 13 and the Z-axis 14. Inaddition, the Y-axis 13 is orthogonal or approximately orthogonal to theZ-axis 14. The first coordinate system 5 provides a mechanism tospatially define the relative location and orientation of elements inthe system of platforms 1500. While the origin 10 may be defined at anylocation within or about the SDA 110, the origin 10 is preferablylocated at the phase center of the N antenna arrays forming the SDA 110.

Similarly, the set of forward-based platforms 700 a-700 n forms asecondary spatially-distributed architecture of antenna arrays 1510 thatidentifies a secondary second coordinate system 5′. In the illustratedembodiment, the second coordinate system 5′ is shifted or translated inone or more of the X, Y and Z directions with respect to the firstcoordinate system 5 defined by the SDA 110. In the illustratedembodiment the X, Y and Z directions of the separate coordinate systemsare parallel to one another. This relationship reduces the complexity ofcoordinate system translations. However, the system of platforms 1500 isnot so limited and other spatial orientations (relationships) arepossible and contemplated.

In the present embodiment the SDA 110 may be a fixed station on theground or a moving station disposed on a moving platform such as, forexample, a ship, an airplane, a flying drone, a truck, a tank, or anyother type of suitable vehicle (not shown). The SDA 110 and the receiversubsystem 130 operate as described in association with the embodimentillustrated in FIG. 1. Together, the SDA 110 and the receiver subsystem130 determine a position of the interceptor platform(s) 700 a-700 n inthe coordinate system 5. As further described above the interceptorplatforms 700 a-700 n may be arranged to self-determine a respectivelocation, orientation and motion (if any) in the coordinate system 5.

In the example embodiment illustrated in FIG. 15, the forward-basedplatform 700 a is arranged with processing circuitry or a processor 751,memory 755, one or more antennas 752, one or more antennas 754,transceiver 753, a guidance system 756 and a signal generator 757. Theforward-based platform 700 a may be fixed to one or more of a missile, aprojectile, a ship, an airplane, a flying drone, a truck, a tank, or anyother type of suitable vehicle or even a relatively small portabledevice (not shown). The forward-based platform 700 a may be locatedwithin line-of-sight of the non-cooperative object or target 120, whilethe SDA 110 and the receiver 130 are not.

When the forward-based platform 700 a is coupled to or part of aprojectile, the platform 700 a may be dropped, launched, expelled orotherwise separated from a ship, airplane, drone, or land-based vehicle.The guidance system 756 is arranged with one or more control systems, aninertial navigation system and is optionally arranged with a propulsionsystem. The one or more antennas 752 receive the N uniquely codedtransmit signals 113 transmitted by the SDA 110. The memory 755 includesone or more logic modules and data values (not shown) that whencontrollably retrieved and executed by the processor 751 enable theprocessor 751, in response to information derived from the N uniquelycoded signals 113 as received at the antennas 752, to self-determine aposition of the forward-based platform 700 a in the coordinate system 5.Changes in the location of the platform 700 a relative to the SDA 110may also be determined by the processor 751 or may be determined solelyin an inertial navigation system (INS) coupled to or otherwise providedin the guidance system 756. As illustrated in FIG. 15 the INS may berelied on to define a second coordinate system 5′ with an origin 10′coexistent or co-located with one or more physical surfaces of theinterceptor platform 700.

The forward-based platform(s) 700 a-700 n are provided with the signalgenerator 757 to create and forward a modulated signal to the one ormore antennas 754. The modulated signal may be bandwidth filtered andupconverted in frequency in the transceiver 753 before beingcommunicated to and transmitted by the one or more antennas 754. Themodulated signal is uniquely associated with the respective instance ofthe forward-based platform 700 a-700 n. As indicated in FIG. 15, Muniquely coded transmit signals 1413 are transmitted toward thenon-cooperative object or target 120 and Q reflected versions of the Munique platform transmitted signals 1414 are reflected back to the oneor more antennas 754. As described in connection with the embodimentillustrated in FIG. 1, time of arrival and phase differences identifiedin the Q reflected versions of the M uniquely coded or uniquelyidentifiable platform generated signals may be processed in theprocessor 751 to determine a range and vector direction in thecoordinate system 5′.

Thereafter, processor 751 in communication with a platform receiver 754determines one or more a position, motion and an orientation of theplatform 700 a in a coordinate system 5′ defined by the platform 700 a.In this regard, the platform 700 a may be relying on informationprovided by an INS in a guidance control system or guidance andpropulsion system 756. Such an INS may provide inaccurate positionalinformation in any one or more of the X, Y and Z axes. When the INS isused as a basis for establishing the coordinate system 5′, erroneous INSinformation will result in additional errors if the position of platform700 a is used to direct or assist one or more platforms 700 n withrespect to the non-cooperative object or target 120. Accordingly, thepilot platform 1445 periodically sends one or more information signals115 containing a present location of the pilot platform 1445 in thecoordinate system 5 to the platform 700 a. In response, the processor751 executes software or firmware that together with the location dataand characteristics of the N uniquely coded transmit signals 113identifies when the INS information in the guidance system 756 is inneed of correction. When this is the case, the location of the platform700 a is replaced.

The same principles described above with reference to FIGS. 5-9 apply tothe operations performed by the platforms to self-track while alsotracking the non-cooperative object or target 120. Alternatively, asignal or signals from a forward-based platform and/or a separate anddistinct system may provide information about the location of a target.

In addition, when platforms 700 a-700 n are configured with antennaarrays 754 arranged to transmit the locally generated uniquely codedsignals from the signal generator 757 these signals produce a remote orsecond or secondary spatially-distributed architecture of antenna arrays1510 different from the (first or primary) SDA 110 in the pilot platform1445. The remote or secondary SDA of antenna arrays 1510 in conjunctionwith a set of uniquely identifiable signals transmitted from each of theseparate antenna arrays can be used to guide or navigate one or moreinterceptor platforms 150 a-150 n when so desired.

Such forward-based platforms 700 a-700 n and interceptor platforms 150a-150 n may share information concerning the location, orientation andmotion (if any) of the non-cooperative object in addition to informationconcerning their respective location in either the coordinate system 5defined by the primary spatially-distributed architecture of antennaarrays 110 or the coordinate system 5′ defined by the secondaryspatially distributed architecture of antenna arrays 1510 as desired. Atwo-way radio-frequency communication channel 1520 is arranged tosupport such transfers of information including location, orientationand motion of the non-cooperative object and/or a respectiveself-determined location, orientation and motion of a platform betweenone or more forward-based platforms 700 a-700 n and one or moreinterceptor platforms 150 a-150 n.

It should be noted that this disclosure has been presented withreference to one or more exemplary or described embodiments for thepurpose of demonstrating principles and concepts. The claimed systems,methods and computer-readable media are not limited to these exampleembodiments. As will be understood by persons skilled in the art, inview of the description provided herein, many variations may be made tothe example embodiments described herein and all such variations arewithin the scope of the invention. For example, a function or capabilityintroduced and described in association with one of the exemplaryembodiments may be introduced or applied in other arrangements whereimprovements to platform guidance or navigation may be desired.

REFERENCE SYMBOLS

-   5, 5′ coordinate system-   10, 10′ origin-   12, 12′ X-axis-   13, 13′ Y-axis-   14, 14′ Z-axis-   100 environment-   110 spatially-distributed architecture-   110′ spatially-distributed architecture-   111 signal generator-   112 N antenna arrays-   113 N uniquely coded signals-   114 reflections (of coded signals)-   115 information signal-   117 N uniquely coded signals (modified)-   120 non-cooperative object (target)-   122 cooperative object-   130 first receiver subsystem-   131 processor-   132 antenna(s)-   135 memory-   138 signal generator-   139 connection-   140 signal-   150 platform(s)-   151 processor-   152 antenna(s)-   154 antenna (optional)-   155 memory-   180 alternate signal source-   185 information signal-   201 SDA subsystem-   202 processor-   203 input/output interface-   204 clock generator-   205 memory-   206 bus-   211 signal generator-   212 Local info. store-   213 TX module-   214 RX module-   215 code store/signal gen.-   216 connection-   217 connection-   220 SDA circuitry-   220′ SDA circuitry-   221 TX circuitry-   221′ TX circuitry-   222 RX circuitry-   223 master oscillator-   224 synchronization clock-   225 connection-   226 TX signal generator-   228 N antenna arrays-   330 receiver platform-   330′ receiver platform-   331 processor-   331′ processor

REFERENCE SYMBOLS (continued)

-   333 input/output interface-   334 clock generator-   335 memory-   336 location module-   337 motion module-   338 information signal logic-   339 local info store-   342 connection-   350 demodulator-   360 matched filter bank-   400 platform-   400′ platform-   402 phase-locked loop (PLL)-   404 local oscillator-   405 summing node-   406 clock-   410 RX/demodulator-   411 processor-   411′ processor-   412 bus-   413 input/output interface-   414 clock generator-   415 memory-   416 connection-   417 connection-   420 matched filter bank-   431 location module-   432 motion module-   433 orientation module-   434 second module (nay./guidance)-   435 signal generator-   436 conversion module-   437 coordination module-   438 local info store-   450 platform circuitry-   460 receiver-   465 antenna-   500 platform-   551 processor-   552 antenna/rcvr.-   553 transceiver circuitry-   554 ant./rcvr. (opt.)-   555 memory-   556 guidance system-   600 a-600 n platform(s)-   700 a-700 n platform(s)-   751 processor-   752 antenna/rcvr.-   754 antenna/rcvr.-   755 memory-   756 guidance system-   757 signal generator-   910 RX array (center)-   1000 SDA method-   1002-1008 method steps-   1100 platform method-   1102-1110 platform steps-   1200 platform method-   1202-1216 platform steps-   1300 platform method

REFERENCE SYMBOLS (continued)

-   1302-1316 platform steps-   1400 system of platforms-   1402 electromagnetic energy-   1404 reflected electromagnetic energy/signal-   1405 target vector-   1413 M coded TX signals-   1414 Q reflections of M Tx signals-   1415 platform vector-   1420 information signal-   1445 pilot platform-   1460 sensor/sensor subsystem-   1500 system of platforms-   1510 secondary SDA of antenna arrays-   1520 two-way communication channel

What is claimed is:
 1. A method, comprising: receiving, with a firstreceiver connected to a platform, a set of uniquely identifiable signalstransmitted from respective spatially-distributed antenna arraysseparate from the platform; determining, with a platform processor incommunication with the first receiver, one or more of a position, amotion and an orientation of the platform in a first coordinate system,wherein the platform processor identifies at least one of the position,motion and orientation of the platform using one or more characteristicsof the uniquely identified signals received by the first receiver;receiving one or more signals containing information about a position ofa non-cooperative object, wherein the information about the position ofthe non-cooperative object is communicated in an established inertialframe or the first coordinate system defined by thespatially-distributed antenna arrays; generating, with the platformprocessor, a guidance solution responsive to the position of thenon-cooperative object with respect to the platform; and applying atleast one control signal responsive to the guidance solution to directthe platform relative to the non-cooperative object.
 2. The method ofclaim 1, wherein receiving one or more signals includes a signalreflected from or a signal originating from the non-cooperative objectand in the case of a signal reflected from non-cooperative object theposition of the non-cooperative object relative to the platform isdetermined from characteristics of the reflected signal.
 3. The methodof claim 1, further comprising: generating, with a transceiver connectedto the platform, a platform unique signal different from any member ofthe set of uniquely identifiable signals transmitted from the SDA ofantenna arrays; transmitting the platform unique signal; periodicallytransmitting a respective informational signal identifying a presentlocation of the platform; and periodically transmitting a respectiveinformational signal identifying a present location of thenon-cooperative object.
 4. The method of claim 3, wherein receiving oneor more signals containing information about a position of anon-cooperative object includes receiving one or more reflected versionsof the set of uniquely identifiable signals transmitted by thespatially-distributed antenna arrays, one or more reflected versions ofthe platform unique signal, or one or more reflected versions of auniquely identifiable signal transmitted from a cooperative object. 5.The method of claim 1, wherein receiving one or more signals containinginformation about a non-cooperative object includes receiving, one ormore signals directly from one or more of the spatially-distributedantenna arrays, one or more signals directly from an alternative signalsource, or one or more signals directly from a cooperative object. 6.The method of claim 1, wherein the guidance solution identifies a rangeand an angle using the position of the platform and the position of thenon-cooperative object.
 7. The method of claim 1, further comprising:periodically receiving a respective informational signal identifying apresent location of one or more of the antenna arrays of thespatially-distributed antenna arrays; and adjusting a present locationof the platform responsive to the present location of the one or moreantenna arrays of the spatially-distributed antenna arrays and aplatform determined position from one or more characteristics of theuniquely identified signals received by the first receiver.
 8. Themethod of claim 7, wherein adjusting a present location of the platformincludes modifying one of a present location, motion, or orientationinformation in an inertial navigation system connected to the platform.9. The method of claim 7, further comprising: communicating, from theplatform, an informational signal identifying one of a location or acomponent of the location of the non-cooperative object.
 10. The methodof claim 1, further comprising: periodically receiving a respectiveinformational signal identifying a present location of one or morecooperative objects; generating, from the platform, a guidance ornavigation solution responsive to the present location of a respectivecooperative object with respect to the non-cooperative object.
 11. Aplatform, comprising: a first antenna arranged to directly receive a setof uniquely identifiable signals transmitted from a respective set ofspatially-distributed antenna arrays; a transceiver coupled to the firstantenna, the transceiver arranged to convert electromagnetic energyresponsive to the set of uniquely identifiable signals to a first set ofcorresponding input signals; and a processor coupled to the transceiverand arranged to use a respective time of arrival and phase from the setof corresponding input signals to determine at least a position of theplatform in a first coordinate system defined by the set ofspatially-distributed antenna arrays; wherein the processor receivesinformation concerning a non-cooperative object.
 12. The platform ofclaim 11, wherein the processor determines a vector in a direction fromthe platform toward the non-cooperative object and wherein thetransceiver and first antenna are configured to transmit a signalrepresentative of the vector.
 13. The platform of claim 12, furthercomprising: an inertial navigation system configured to provideposition, orientation and velocity of the platform to the processor,wherein the processor generates a guidance solution responsive to theposition, orientation, and velocity of the platform and the vector todirect the platform relative to the non-cooperative object.
 14. Theplatform of claim 12, wherein the platform receives a corrective signalfrom a remote processor coupled to the spatially-distributed antennaarrays and controllably applies the corrective signal to the inertialnavigation system.
 15. The platform of claim 14, wherein the processorapplies the corrective signal to the inertial navigation system inresponse to a comparison of the position and velocity of the platform asprovided by the inertial navigation system with the position andvelocity of the platform as determined by a remote processor responsiveto reflected versions of the set of uniquely identifiable signals.
 16. Asystem, comprising: a set of cooperative platforms separate from aprimary spatially-distributed architecture of antennas, the primaryspatially-distributed architecture of antenna arrays configured to emita set of uniquely identifiable signals; members of the set ofcooperative platforms configured to receive: the set of uniquelyidentifiable signals from the primary spatially-distributed architectureof antenna arrays; and one or more signals containing information abouta position of one or more non-cooperative objects, wherein theinformation about the positions of the non-cooperative objects arecommunicated in an established inertial frame or in a first coordinatesystem defined by the primary spatially-distributed architecture ofantenna arrays; members of the set of cooperative platforms furtherconfigured to: determine a respective location in one of the establishedinertial frame or in the first coordinate system defined by the primaryspatially-distributed architecture of antennas; and apply a respectiveplatform control signal to direct the respective platform relative tothe non-cooperative object.
 17. The system of claim 16, wherein thecooperative platforms determine respective locations in the firstcoordinate frame using the set of uniquely identifiable signals andcommunicate the locations to the platform.
 18. The system of claim 16,wherein at least one of the members of the set of cooperative platformsis configured to determine the location of the non-cooperative objectand transmit the one or more signals containing information about theposition of the non-cooperative object.
 19. The system of claim 16,wherein the non-cooperative objects are selected from a group consistingof vehicles, ships, buoys, flotsams and jetsams, wherein a cooperativeplatform is selected from a group consisting of vehicles, ships, andbuoys and the control signal is responsive to a desired course of theplatform.
 20. The system of claim 18, wherein the at least one member ofthe set of cooperative platforms is further configured to generate andtransmit the respective platform control signal to one or more remainingmembers of the set of cooperative platforms.
 21. The system of claim 16,wherein one or more of the members of the set of cooperative platformsare further configured to generate and transmit a respective cooperativeplatform unique signal to determine the location of the non-cooperativeobject.
 22. The system of claim 16, wherein the one or more signalscontaining information about a position of a non-cooperative objectinclude one or more signals received directly from the primaryspatially-distributed architecture of antenna arrays, an informationsignal from an alternative signal source, a signal originating from thenon-cooperative object, a signal from one of the remaining members ofthe set of cooperative platforms, or a reflected version of a respectiveplatform unique signal.
 23. The system of claim 16, wherein thecooperative and non-cooperative objects are selected from a groupconsisting of drones, projectiles, missiles, aircraft, and spacecraftand the control signal is responsive to a desired course of therespective platform.
 24. The system of claim 16, wherein at least two ormore members of the set of cooperative platforms are configured todetermine a component of the position of the non-cooperative object. 25.The system of claim 24, wherein the component of the position of thenon-cooperative object and a respective location of the cooperativeplatforms are shared with one or more of the cooperative platforms whichare configured to determine and communicate the location of thenon-cooperative object in the first coordinate system.